An O(N) algorithm for Stokes and Laplace interactions of particles

Size: px
Start display at page:

Download "An O(N) algorithm for Stokes and Laplace interactions of particles"

Transcription

1 Syracue Unverty From the SelectedWork of Ahok S. Sangan 1996 An O(N) algorthm for Stoke and Laplace nteracton of partcle Ahok S. Sangan, Syracue Unverty Guobao Mo, Syracue Unverty Avalable at:

2 An O(N) algorthm for Stoke and Laplace nteracton of partcle Ahok S. Sangan and Guobao Mo Ctaton: Phy. Flud 8, 1990 (1996); do: / Vew onlne: Vew Table of Content: Publhed by the Amercan Inttute of Phyc. Related Artcle Cloud of partcle n a perodc hear flow Phy. Flud 24, (2012) The dynamc of a vecle n a wall-bound hear flow Phy. Flud 23, (2011) A tudy of thermal counterflow ung partcle trackng velocmetry Phy. Flud 23, (2011) Partcle accumulaton on perodc orbt by repeated free urface collon Phy. Flud 23, (2011) Drag force of a partcle movng axymmetrcally n open or cloed cavte J. Chem. Phy. 135, (2011) Addtonal nformaton on Phy. Flud Journal Homepage: Journal Informaton: Top download: Informaton for Author:

3 ARTICLES An O(N) algorthm for Stoke and Laplace nteracton of partcle Ahok S. Sangan a) and Guobao Mo Department of Chemcal Engneerng and Materal Scence, Syracue Unverty, Syracue, New York Receved 27 December 1995; accepted 12 Aprl 1996 A method for computng Laplace and Stoke nteracton among N phercal partcle arbtrarly placed n a unt cell of a perodc array decrbed. The method baed on an algorthm by Greengard and Rokhln J. Comput. Phy. 73, for rapdly ummng the Laplace nteracton among partcle by organzng the partcle nto a number of dfferent group of varyng ze. The far-feld nduced by each group of partcle expreed by a multpole expanon technque nto an equvalent feld wth t ngularte at the center of the group. The reultng computatonal effort ncreae only lnearly wth N. The method appled to a number of problem n upenon mechanc wth the goal of aeng the effcency and the potental uefulne of the method n tudyng dynamc of large ytem. It hown that reaonably accurate reult for the nteracton force are obtaned n mot cae even wth relatvely low-order multpole expanon Amercan Inttute of Phyc. S I. INTRODUCTION a Electronc mal: aangan@malbox.yr.edu Numercal mulaton of moton of partcle through a upendng flud provde valuable nght nto the complex nterrelatonhp between the mcrocale phyc, the mcrotructure, and the macrocopc behavor of upenon. However, the problem of determnng hydrodynamc nteracton among many partcle computatonally ntenve wth mot of the extng method for mulaton utable only for a relatvely mall number of nteractng partcle, typcally of O(100). Whle th adequate for many problem, there are alo large number of problem for whch t derable to mulate ytem contanng much greater number of partcle. For example, the unform tate of mall Reynold number, fnte Stoke number, ga-old fludzed bed known to be untable for certan range of t parameter the volume fracton of the partcle and the Stoke number reultng n the formaton of large bubble or regon devod of partcle. Large-cale mulaton are needed to undertand n detal the mechanm reponble for thee macrocopc ntablte. Smlarly, problem nvolvng concentrated fber upenon wth nl 3 of O( ) requre large-cale mulaton nvolvng thouand of fber n order that the box ze ued n the mulaton doe not gnfcantly affect the behavor of uch upenon. Here, n the number denty of fber and l the length of fber. Moreover, recent expermental and numercal work on edmentng fber ugget that the unform tate of uch upenon untable reultng n the formaton of cluter. 1 Large-cale mulaton are needed to determne the cluter ze dtrbuton and the reultng properte of the edmentng fber upenon. Large-cale mulaton are alo needed n the tudy of upenon wth gnfcant wall effect, polydpere upenon, or for upenon n whch the hydrodynamc nteracton are expected to be creened at dtance large compared to the ze of the partcle. Two maor dffculte n computng hydrodynamc nteracton among partcle n Stoke mall Reynold number flow are: the long-range, multpartcle nature of nteracton; and the lubrcaton effect arng from a relatve moton of partcle n cloe proxmty to each other. Thee are explaned n more detal below. The velocty dturbance caued by a partcle wth a net nonzero force actng on t decay only a 1/r, r beng the dtance from the center of the partcle, and therefore t not poble to ue an arbtrary cut-off radu for truncatng the hydrodynamc nteracton among partcle. In other word, one mut compute the nteracton among all the partcle n the upenon. The velocty nduced by a partcle generally expreed n term of a dtrbuton of hydrodynamc force denty actng along t urface. The multpartcle nature of the nteracton are due to the fact that th force denty unknown and to be determned a a part of the oluton by olvng for the force denty on all the partcle multaneouly. Th dfferent, for example, from the problem of computng Coulombc nteracton among pece wth known charge for whch the nteracton are alo longranged but, becaue the charge on the ndvdual pece known, the nteracton are par-addtve. A a conequence, no mple par-addtve approxmaton can be made n computng hydrodynamc nteracton. When two partcle n cloe proxmty approach toward each other wth an O(1) relatve velocty, the flud n the gap between the partcle mut queeze out radally from the narrow gap between the partcle. Th reult n a radal velocty of O( 1/2 ) n the gap regon of thckne and a force denty of O( 2 ) localzed to an O() urface area of each partcle. Th known a the lubrcaton effect. See, for 1990 Phy. Flud 8 (8), Augut /96/8(8)/1990/21/$ Amercan Inttute of Phyc

4 example, Happel and Brenner 2 or Km and Karrla 3 for detal. Snce the lubrcaton force denty hghly localzed to a relatvely mall area of the the urface of the partcle, the conventonal numercal technque, uch a the boundary ntegral technque n whch the urface of the partcle dcretzed nto a number of urface element ee Pozrkd 4 for detal, become mpractcal for large ytem a the number of dcretzed element needed for reolvng the lubrcaton effect become prohbtvely large a the two partcle approach each other. To overcome the above two dffculte, Brady and Bo 5 deved an ngenou cheme n whch the manypartcle retvty matrx, whch gve the force denty on the partcle gven ther velocte, expreed a a um of far-feld approxmaton to the many-partcle moblty matrx nvere and the par retvty tenor. The former account for the long-range, multpartcle nature of the nteracton whle the latter account for the lubrcaton force between par of partcle whch contrbute n a par-addtve manner to the retvty tenor. Th method alo ued by Ladd 6 who howed that the approxmaton deved by Brady and Bo can be ytematcally mproved by ncludng hgherorder approxmaton to the far-feld moblty matrx. The man advantage of the method over the conventonal boundary ntegral method that relatvely few unknown typcally 11 to 26 per partcle are needed for determnng manypartcle nteracton wth an accuracy that adequate for many dynamc mulaton problem. 5,6 Unfortunately, the method requre nvertng a far-feld moblty matrx wth at leat (11N) 2 element, the computatonal effort for whch grow a N 2 a the ytem ze ncreae, N beng the number of partcle n the ytem. Th lmt the computaton to N of no more than few hundred. Alternate method that do not requre nvertng the moblty matrx have been propoed by Mo and Sangan, 7 Sangan and Mo, 8 and Cchok et al. 9 Cchok et al. employed the ame dea a Brady and Bo to account for the lubrcaton effect but avoded the matrx nveron wth the help of a utable tranformaton of the equaton governng the multpole. In the preent tudy we ue the method propoed by Sangan and Mo. Accordng to th method, the force denty on the partcle decompoed frt nto a lubrcaton force denty whch localzed to the gap regon between the cloely paced partcle and a regular force denty whch dtrbuted on the entre urface of the partcle. The velocty due to the latter expreed n term of force multpole at the center of the partcle whle that due to the former approxmated n term of a force dpole at the center of the gap between the partcle. Th method thu account for both the long-range, multpartcle nature of the nteracton and the lubrcaton effect. Applcaton of the boundary condton on the urface of the partcle lead to a ytem of lnear equaton of the form A xb, where x a vector of tranlatonal and rotatonal velocty of the partcle and the nduced force multpole, A an O(NN) matrx and b a vector that depend on the mpoed flow. In Sangan and Mo, 8 each element of the matrx A wa evaluated eparately and the reultng equaton were olved ubequently to determne the force multpole and the velocte of the partcle. The accuracy of the method wa hown to be comparable to that of the method of Brady and Bo. 5 However, nce each element of A wa evaluated eparately, the method alo requred O(N 2 ) computaton, and, conequently, no gnfcant computatonal avng reulted even though t avoded the computaton of the moblty matrx nvere. For large ytem, t wll be advantageou to deve cheme n whch the computatonal effort ncreae much more lowly wth N. The oluton of the et of lnear equaton A xb typcally obtaned by teratve method when N large. In order that th can be accomplhed wth only an O(N) computatonal effort, one mut be able to compute A x for a gven x n an O(N) tme. Th the man obectve of the preent nvetgaton. Our method baed on a fat ummaton technque baed on herarchal groupng of partcle developed for computng Coulombc and gravtatonal nteracton. There are everal way of dong th ee, for example, Apple, 10 Barne and Hut, 11 and Greengard and Rokhln. 12 Here, we hall follow the approach outlned by Greengard and Rokhln. 12 Thee nvetgator and the other co-worker of Greengard have developed an algorthm for computng Laplace and Coulombc nteracton n the twoa well a three-dmenonal pace 13,14 and for the elatc nteracton n the two-dmenonal pace. 15 The feld created by a group of partcle far from a gven partcle expreed n term of multpole at the center of the group a decrbed n more detal later n th paper. Snce the feld repreented by a group of partcle wth a fxed number of multpole become accurate when the dtance from the center of the group large compared wth the lnear dmenon of the group ze, we need a herarchy of group n whch the feld felt by a gven partcle evaluated by ung maller group of partcle that are relatvely cloe to the partcle and larger group of partcle that are further away from t. The method decrbed by Greengard and Rokhln for olvng Laplace equaton tart wth a dcretzaton of the boundary ntegral and th make t omewhat neffcent for treatng upenon problem n whch the lubrcaton force are gnfcant. Although the computatonal effort cale lnearly wth N, the number of dcretzaton element per partcle wll be prohbtvely large when the lubrcaton effect are gnfcant. However, by combnng ther technque of rapdly ummng the nteracton wth the method of Sangan and Mo, 8 n whch the number of unknown per partcle mall due to explct treatment of the lubrcaton effect, t hould be poble to decreae the overall computatonal effort gnfcantly. Alo, a we hall ee, the extenon of the method to um Stokean nteracton nontrval. The method requre developng approprate expreon for the far-feld and near-feld repreentaton of the feld nduced by a group of partcle. Greengard and Rokhln gave thee expreon for the Laplace equaton and the preent tudy derve mlar relaton for the Stoke equaton. The method appled to everal problem to ae the effcency and the potental uefulne of the algorthm. We hould perhap menton here about an O(N) algorthm baed on the lattce-boltzmann ga technque that already ext for the tudy of hydrodynamc nteracton n Phy. Flud, Vol. 8, No. 8, Augut 1996 A. S. Sangan and G. Mo 1991

5 upenon. The flud contnuum n Stoke nteracton replaced by a lattce-boltzmann ga wth approprate rule for t molecule to exchange ther poton and momentum. It found that wth utable rule for th exchange n the bulk and at the nterface between the partcle and the molecule of the lattce-boltzmann ga, t poble to mmc the behavor of rgd partcle upended n a Naver Stoke flow. A method baed on th dea ha been extenvely teted n two recent paper by Ladd. 16,17 Ladd ha been able to carry out Stokean dynamc mulaton of upenon wth N of O(10 4 ) ung th technque. In addton to beng O(N) n computaton, the method ha the advantage of beng able to treat both the nonzero Reynold number flow pat fxed partcle and the upenon of ubmcron zed partcle for whch the Brownan force are gnfcant. Th method, however, tll n t early tage of development wth t accuracy and effcency for large N ytem unteted and unchallenged by the other drect approache baed on olvng partal dfferental equaton arng from the contnuum approxmaton. It hoped that n the leat the method developed here may erve a a check and an alternate to the lattce-boltzmann ga baed algorthm for monodpere upenon of rgd partcle. Furthermore, nce the ze of the lattce typcally governed by the mallet dmenon of the partcle, t appear that the method of ummng nteracton by herarchal groupng wll be far more effcent n dealng wth the upenon of lender fber or polydpere upenon. Alo, nce n general, t a nontrval tak to determne the approprate rule for the exchange of momentum at the nterface to mmc boundary condton other than the no-lp condton, t expected that the method decrbed n th paper wll be more readly adapted to the upenon of charged partcle, 18 drop or bubble. 7 Note that for hghly deformable partcle and lender fber, the nteracton can be computed ung the ntegral equaton repreentaton for the Stoke flow ntead of the multpole repreentaton. The lubrcaton effect mentoned earler lkely to play le mportant a role for thee cae, and conequently the traghtforward ntegral equaton coupled wth the fat ummaton method decrbed here expected to be adequate for the tudy of uch upenon. The bac method outlned n Sec. II where we conder a mple cae of Laplace nteracton. We have choen to treat thee nteracton frt nce the method much eaer to undertand for th cae and becaue of t applcaton to the mulaton of bubbly lqud at large Reynold and mall Weber number ee Sangan and Ddwana 19. Although the general prncple are the ame a n the method outlned by Greengard and Rokhln, the detal are qute dfferent. In Sec. III we decrbe the method for computng Stoke nteracton. In Sec. IV we ae the effcency of the algorthm by applyng t to a number of problem. Frt we conder two Laplace nteracton problem: determnaton of the effectve reacton rate contant n a dffuon-lmted reactng medum; and determnaton of the added ma coeffcent for partcle n nvcd upenon. Next, we conder three Stoke flow nteracton problem: a unform flow through fxed bed of partcle; effectve vcoty of upenon; and edmentaton velocty and hydrodynamc fluctuaton n upenon. II. THE METHOD FOR LAPLACE INTERACTIONS A mentoned n Sec. I, we hall frt conder a mpler problem of determnng Laplace nteracton of phercal partcle. We hall explan the method n reference to a problem of dffuon-controlled reacton. Th wll be applcable wth mnor modfcaton to the other problem of Laplace nteracton. When the ze of one of the reactant pece much greater than the other, the larger pece may eentally be regarded a mmoble and the rate of reacton then depend on the rate at whch the maller pece dffue through the medum and arrve at the urface of the larger, mmoble pece. To model th tuaton, we conder a upenon contng of N phercal partcle each of radu a placed wthn a unt cell of a perodc array. The upendng flud contan a pece wth a lnear dmenon much maller than a whch dffue through the flud wth a contant dffuvty D. The pece react very rapdly wth the phere uch that t concentraton at the urface of the phere may be taken to be vanhngly mall. We hall aume that the pece contnuouly produced n the flud at a contant rate throughout the flud medum. At teady tate the average concentraton C of the pece n the upenon determned by the balance between the rate at whch t produced n the bulk and the rate at whch t conumed by the reacton. The problem then to determne the non-dmenonal reacton rate contant R defned by Q4aDR C. 1 Here, Q the average quantty of the pece reactng per unt tme on a ngle phere. When, the volume fracton of the phere, mall, the nteracton among phere can be neglected, and R 1 a reult frt gven by Smoluchowk. 20 An etmate of the frt correcton for mall but fnte wa gven by Felderhof and Deutch, 21 and, more recently, numercal mulaton have been ued to compute R a a functon of for dene upenon ee, for example, Felderhof 22. Our goal wll be to calculate R for a few elected confguraton of N phere. The flud aumed to be at ret o that the pece concentraton C atfe the Poon equaton 2 CS0 wth the boundary condton C0 on the urface of the phere. Here, DS the net rate at whch the pece produced per unt volume of the flud and related to Q by DS(1)nQ, n beng the number denty of the phere. It may be noted that the preence of S n Eq. 2 render t a Poon equaton ntead of the Laplace equaton but we hall contnue to refer to the nteracton a Laplacan nce Eq. 2 a rather trval pecal cae of the more general Poon equaton n whch the nk term a functon of the poton. In Sec. IV, where we preent the reult of computaton for R, we hall alo conder the problem of Phy. Flud, Vol. 8, No. 8, Augut 1996 A. S. Sangan and G. Mo

6 added ma whoe governng dfferental equaton ndeed the Laplace equaton, and the oluton for that cae wll be obtaned mply by ettng S0. A. A revew of an O(N 2 ) algorthm Before decrbng the O(N) algorthm n detal, t ueful to preent a more conventonal method of multpole expanon n whch the computaton grow a N 2 a the ytem ze ncreaed. The method ha a cloe connecton to the boundary ntegral method but enoy an advantage of a fater convergence for mple partcle hape uch a phere condered n the preent tudy. Th method wa outlned n reference to the problem of determnng the effectve thermal conductvty and the added ma coeffcent for a gven confguraton of phere n our earler tude. 23,24 The concentraton C of the dffung pece can be expreed n term of the Green functon or the fundamental ngular oluton S 1 of the Poon equaton a N CxC 1 G S 1 xx, 3 where C to be choen uch that the average concentraton equal C, G a dfferental operator that wll be defned more precely later n the ecton, x the center of the partcle, and S 1 the patally perodc Green functon atfyng 2 S 1 x4 1 xl xx L. 4 Here, x L repreent the lattce pont of the perodc array, the volume of the unt cell of the perodc array, and the Drac delta functon. The contant nk term 1 n the above expreon needed to balance the ource term at the lattce pont. An Ewald technque for evaluatng S 1 decrbed n detal by Hamoto. 25 More detal ncludng expreon for the dervatve of S 1 are gven n Sangan et al. 24 and Cchok and Felderhof. 26 A hown by Hamoto, S 1 (x) ha a ngular, ource-lke, behavor near lattce pont where t behave a 1/xx L. The ue of patally perodc Green functon enure that the feld nduced by each partcle,.e., G S 1 (xx ), patally perodc, and hence content wth the mpoed perodc boundary condton. Thu, we only need to atfy the boundary condton at the urface of the partcle. For the cae of phercal partcle t convenent to expre C near each partcle n term of phercal harmonc n a polar coordnate ytem wth t orgn at the center of that partcle. Thu, near partcle, we expre C a 1 CSr 2 /6 0 n0 where rxx, and wth n m0 E, nm A, nm r 2n1 r, 5 are the old phercal harmonc Y 0 nm r n P m n com, Y 1 nm r n P m n nm. 6 Here, co and the phercal polar angle and are defned by r 1 rco, r 2 rnco, and r 3 rnn. Now the boundary condton of vanhng C at ra yeld E, nm a 2n1 A, nm 1 6 Sa2 n0 m0 0 0, where n0 a Kronecker delta functon whoe value unty for n0 and zero otherwe. In order that Eq. 3 can be recat nto Eq. 5, we defne the dfferental operator G uch that the ngular term at x n Eq. 3 are exactly the ame a thoe n Eq. 5. Snce the ngular part of S 1 equal 1/r, we requre that G r 1,n,m r 2n1 A nm, 7, 8 where the ummaton over,n,m the ame a that n Eq. 5. In Appendx A, we have compled a number of ueful reult on the dfferentaton of 1/r and the other phercal harmonc. Ung Eq. A1, we ee at once that G,n,m 1 nm A, nm D nm, 9 where nm gven by Eq. A2 and D nm the dfferental operator defned by Eq. A3. The contant A, nm wll be referred to a the nduced multpole. Now the coeffcent E, nm of the term that are regular at r0 n Eq. 5 are related to the nth order dervatve of the regular part of C at r0 bycf. Eq. A6-A8 E, nm nm D nm C reg Sr 2 /6 r0, 10 where nm gven by Eq. A8 and C reg equal C mnu the ngular part at r0,.e. C reg CG r 1. Subttutng for G from Eq. 9 nto Eq. 3 and combnng t wth Eq. 10 yeld E, nm nmd nm k 1 N l0 k0 0 1 C Sr 2 /6 r0 1 kl A kl, D nm D kl S 1 x x, 11 where the ngular part 1/r mut be removed from S 1 before dfferentatng t for. For later reference, we note that S related to the um of monopole by mean of a mple relaton N S 4 1 0, A obtaned by combnng Eq. 4 and 9. Here, we made ue of the fact that all ngularte are tuated nde the partcle o that, for a pont lyng n the flud, Eq. 4 mplfe to 2 S 1 4/. Now the O(N 2 ) algorthm cont of truncatng the nfnte et of equaton repreented by Eq. 7 and 11 by conderng only the equaton and multpole A, nm wth nn. Th reult n a total of N t N(N 1) 2 number of equaton n an equal number of unknown multpole A, kl. Thee equaton are cat nto a form A xb where x an Phy. Flud, Vol. 8, No. 8, Augut 1996 A. S. Sangan and G. Mo 1993

7 N t -vector of unknown multpole trength, A an N t N t matrx whoe coeffcent are the dervatve of S 1 (x x ), and b an N t -vector that related to C, or, equvalently, C. The computatonal cot typcally governed by the calculaton of N t 2 element of the matrx A. Th computatonally ntenve nce S 1 telf to be computed ung ere n real and recprocal pace lattce vector. 25 When hgh accuracy n numercal mulaton not crtcally requred, t poble to avod the repeated calculaton of S 1 for all par of partcle by ung a grd nterpolaton cheme n whch the unt cell frt dvded nto a number of maller cube wth the help of a grd and all the dervatve of S 1 needed n the calculaton are evaluated at the grd pont and tored for the nterpolaton purpoe n the ubequent calculaton. Although th reduce the computatonal effort conderably, the computaton tll grow quadratcally wth N t. The et of lnear algebrac equaton ubequently olved ung an approprate teratve olver and th requre computaton of O(N t 2 ) tme the number of teraton requred for the convergence to wthn a dered accuracy. Thu, the overall computatonal effort and the memory torage for the matrx A) cale a N t 2. In earler calculaton, 8,24 we olved the ytem of equaton ung a Gauan elmnaton algorthm whch requred an O(N t 3 ) effort, but for mall N, the computatonal tme wa motly governed by the tme for computng the matrx element and thu th tep wa not crucal. B. Far- and near-feld repreentaton of the dturbance nduced by a group of partcle In order that the overall computaton for determnng the multpole cale lnearly wth N t, we mut be able to determne E, nm wth O(N t ) computaton. The method decrbed n Sec. II A neffcent for large N t nce t compute the dturbance created by each partcle eparately at the center of each partcle. Clearly, the feld created by partcle that are eparated by a large dtance from partcle can be grouped together for the purpoe of evaluatng ther effect on partcle. Smlarly, all the partcle near feel mlar regular feld (C reg ) from the group of partcle far away from them and therefore the calculaton of the regular feld for the partcle could alo be grouped together. If we mply create all the group of partcle wth each group contanng nearly an equal number P of partcle, then we would requre O((N/P) 2 ) group group nteracton computaton. In addton, we mut eparately account for the nteracton among partcle that are neghbor and th would requre O(NP) computaton reultng n a total computatonal effort that cale roughly a N 2 /P 2 NP. Th ha a mnmum for PO(N 1/3 ), and the total computatonal tme for th optmum P cale a N 4/3. In order to further reduce the order of computaton we mut create a herarchy among group of partcle and adopt a trategy n whch the regular feld near partcle evaluated by combnng greater number of partcle that are further away from t and fewer partcle that are cloer to t. Th can be accomplhed ung the algorthm of Greengard and Rokhln 12 whch we hall preent n more detal n Sec. II C. Here, we hall derve the expreon that are needed for combnng the feld nduced by a group of partcle and the regular feld felt by a group of partcle. In partcular, we need to know how to tranlate a feld nduced due to a ngularty at x c to a feld wth ngularty at another pont x p uch that both feld are dentcal at a pont x uffcently far away from both x c and x p ; and how to tranlate a feld whch regular and expreed n old phercal harmonc at one pont to a regular feld expanded around another pont n t vcnty. The frt one wll be ueful, for example, n combnng the feld nduced by a group of partcle whle the econd one wll be ueful n determnng C reg around a number of partcle near. Greengard and Rokhln accomplhed thee two tak through the ue of addton theorem for Legendre functon. We hall ue a dfferent procedure here, one that we have found more utable to treat the cae of Stoke flow to be condered n Sec. III. Alo, nce the method preented here ncorporate the perodc boundary condton mpoed by the preence of the unt cell at the outet, t ha the advantage of dealng more ealy wth varou knd of non-abolutely convergent um that otherwe are n calculaton nvolvng the Green functon for nfnte doman. The cae of nteracton among fnte number of partcle n an nfnte medum can of coure be trvally recovered by ubttutng 1/r n place of S 1 (r). 1. Tranlaton of ngularte We wh to tranlate a feld C c G c S 1 (xx c ) wth t ngularte at x c to an equvalent feld C p wth t ngularte at x p uch that both C c and C p gve the ame value of C or t dervatve at a pont x far from both x c and x p.we tart wth a Green dentty f 2 CC 2 f dv r V fccf nda r, 13 V where V any volume enclong pont x c and x p, V t urface, n the unt outward normal on V, and rxx p. Now we chooe f to equal (r)(0,1) and ubttute n turn for C both C c and C p. Snce C c C p and C c C p on V, the urface ntegral n both mut be equal and therefore we obtan r 2 C c dv r V r 2 C p dv r, 14 V where we have made ue of the fact that 2 f 2 (r)0. Note that th doe not aume that C c and C p are equal at all pont wthn V, only ther equvalence on V.) Care mut be taken n evaluatng the above ntegral nce the Laplacan of C c or C p a ere n generalzed functon 2 C c G c 2 S 1 rr cp 4A 0,c kl A kl,k,l,c D kl rr cp, Phy. Flud, Vol. 8, No. 8, Augut 1996 A. S. Sangan and G. Mo

8 where r cp x c x p. Here, we have ued Eq. 9 to repreent C c n term of multpole A,c kl at x c and Eq. 4 for the Laplacan of S 1, the pont x c and x p beng aumed to le nde the bac unt cell wth x L 0. Now nce C p mut be patally perodc, the mot general form for t wth ngularte at x p C p e p 1 kl A kl,k,l,p D kl S 1 r, 16 where e p a contant that may are n tranlatng the ngularte from x c to x p, and A,p kl are the multpole at x p. Subttutng Eq. 15 and 16 nto Eq. 14 we obtan 1 n A,p nm nm nm 1 k 1 kl A,c kl D kl,k,l Here, we have ued the reult that D kl r cp. 17 (r) at r0 nonzero only for, nk, and ml, and that t value for th pecal cae 1/ nm. Alo, n dervng the above reult we have aumed that the monopole at x c and x p, are equal,.e., A 0,c 00 A 0,p 00, a reult that verfed a poteror from Eq. 17. Thu, the term contanng 1 n Eq. 4 made no contrbuton to Eq. 17. Fnally, we alo made ue of the followng reult for the ntegraton of generalzed functon: rd kl rr cp dv1 k D kl V r cp. 18 Expreon 17 allow one to compute the multpole at x p gven ther value at x c. A more convenent form that ueful for computng thee multpole can be obtaned by ung the reult gven n Appendx A where we have preented more detaled formulae for evaluatng the dervatve of phercal harmonc. It may be noted that the frt few multpole at x p could alo be obtaned by a traghtforward Taylor ere expanon of C c around x p. Thu, ung G S 1 rr cp GS 1 rr cp GS 1 r..., 19 the relaton among frt few multpole can be readly obtaned A 0,p 00 A 0,c 00, A 0,p 10 A 0,c 10 r cp 1 A 0,c 00, A 0,p 11 A 0,c 11 r pc 2 A 0,c 11, It eay to verfy that thee are n agreement wth the more general reult gven by Eq. 17. Calculaton of hgher-order multpole ung the Taylor ere expanon, however, become cumberome and the method preented here baed on generalzed functon prove more convenent. To complete the tranlaton, we need to determne the contant e p. For th purpoe we tart wth the dentty V C 1 6 r2 2 CdV 3 1 n rc 1 V 2 r2 CdA 21 and once agan ubttute for C n turn both C p and C c. The volume V choen to be the bac unt cell n whch both x c and x p le and V the urface of the unt cell. Snce both C p and C c are requred to be equvalent at all pont on the urface of the unt cell, the urface ntegral n both cae mut be dentcal leadng thereby to the equalty of the volume ntegral cdv C c 1 6 r2 2 C C p 1 6 r2 2 C pdv. 22 Subttutng for C c and C p, notng that the ntegral of G S 1 over the unt cell vanhe, and ung the generalzed functon repreentaton of Laplacan of C c and C p, we obtan e p 2 3 A 20 0,p 2 3 A 00 0,c r pc r pc 2A 0,c 10 r pc 1 2A 0,c pc 11 r 2 2A 1,c 11 r pc 3 A 0,c 20, 23 whch can be further mplfed by ubttutng for A 0,p 20 from Eq. 17 to obtan e p 2 A 00 0,c r pc 2 Y 0 20 r pc 3A 0,c 11 r pc 2 A 1,c 11 r pc 3 24 Equaton 17 and 24 allow u to hft the multpole ngularte at pont x c to that at x p. Thee wll be ueful n combnng the dturbance created a group of partcle nto an equvalent dturbance created at a ngle pont x p. 2. Tranlaton of regular oluton We now conder the problem of tranlatng a feld C reg,p whch regular at both x p and x c thee are not to be confued wth the ngular pont we ued n the prevou dervaton and for whch a phercal harmonc expanon around x p known to the correpondng feld wth t expanon around x c. Let C reg,p 1 6 fr2,n,m E nm,p r 25 be the regular expanon around rxx p 0. We then wh to determne the coeffcent that appear n the expanon around x c C reg,c 1 6 frrcp 2,k,l E kl,c Y kl rr cp. 26 For th purpoe we ue the fact that E kl related to a kth order dervatve of C reg,c evaluated at rr cp E,c kl kl D kl C reg 1 6 frrcp. 27 2rr cp Subttutng for C reg from Eq. 25 we obtan the dered reult E,c kl 1 6 f kld kl r cp 2 2r r cp rr cp kl,n,m E,p nm D kl r cp. 28,c Once agan, expreon for the frt few coeffcent E kl could alo be obtaned ung the Taylor ere expanon, and the reult obtaned that way can be hown to be n agreement wth the above more general reult. Phy. Flud, Vol. 8, No. 8, Augut 1996 A. S. Sangan and G. Mo 1995

9 C. An O(N) algorthm We now decrbe the O(N) algorthm for computng the Laplace nteracton. Th cont of the followng tep: 1 Create a herarchy tree. The frt tep to create a herarchy among group of partcle. For mplcty, we hall aume that our bac unt cell cubc. We dvde th nto 8 equal-zed cube each wth t lnear dmenon half that of the bac cell. Thee are referred to a the level 0 boxe. Next, each box at level 0 further ubdvded nto 8 maller level 1 boxe leadng to a total of 64 boxe at level 1. The proce contnued to the fnet level m lev at whch the box ze uch that on average there are P partcle per fnet level box, P beng a contant of O(1) whoe prece value mut be determned by optmzng the total computatonal tme. Note that there are a total of m lev 1log 8 (N/P) level. Fnally, each partcle agned the fnet level parent box n whch t center le. 2 Upward pa. The econd tep to determne the multpole repreentaton of the feld nduced by a group of partcle that vald at large dtance from the group. It aumed that we hall determne the multpole of the partcle by a utable teratve procedure cf. Step 5. Thu, at the begnnng of each teraton we tart wth the aumed value of the multpole A, nm for each partcle and compute the contrbuton from each partcle multpole to t parent box multpole and the contant e p at m lev level ung Eq. 17 and 24 wth x p n that expreon beng the poton vector of the center of the parent box and x c and A,c kl, repectvely, the center and the multpole of partcle. Next, wth the multpole and the contant e for all the fnet level boxe computed, we determne the multpole and e for the next coarer m lev 1 level boxe wth each parent box multpole now determned from the multpole of t eght chldren at level m lev. Th procedure repeated to larger ze boxe to compute the contant e and the multpole of all the boxe at all the level. 3 Downward pa. The multpole and the contant e determned n Step 2 gve the far-feld repreentaton of the effect of partcle whoe center located n a gven box. We next want to compute f and E kl,.e., the coeffcent that appear n decrbng the regular feld, for all the boxe at all the level. Th acheved by tartng wth the boxe at level 1 or level 0 f the bac unt cell not cubc but oblong ntead, for example and determnng the contrbuton to the regular feld expanon about the center of the boxe from the dturbance due to partcle n the other boxe at the ame level but the one that are not t nearet neghbor. Here, and n the ubequent dcuon, we hall refer to all the 26 nearet neghbor of a gven box at a gven level and the box telf a the nearet neghbor of the box for the ake of brevty. Thu, a gven box ha 27 nearet neghbor. At level 1, there are boxe that are further away from a gven box and contrbuton to f and E kl of a gven box from the partcle n thee 37 boxe can be determned ung Eq. 11 wth the ummaton over n that expreon replaced by the ummaton over thee 37 equal generaton boxe. Of coure, x mut be replaced by the poton vector of the center of the box whoe regular coeffcent are beng computed and x by the center of the equal generaton box from whch the contrbuton beng computed. Alo, S to be ued equal the net nk S eq due to all the partcle repreented by the equal generaton boxe. Th can be determned from Eq. 12 wth the ummaton over once agan replaced by the ummaton over the equal generaton boxe. Now comparng wth the regular expanon gven by Eq. 25, we ee that at th level f for a gven box the um of S eq over t 37 equal generaton dtant neghbor. Next, we compute f and E kl of the boxe at the next fner level,.e., level 2. Unlke level 1, n addton to the contrbuton from t equal generaton level 2 boxe there are equal generaton boxe for each box at th level, we mut alo determne the contrbuton from the regular expanon of t parent box at level 1. Denotng the box at level 2 under conderaton by a upercrpt c, the parent by p, and the equal generaton box by eq, we wrte f c f p S eq, E,c kl E,p c kl eq eq E,eq c kl, 29 and ue Eq. 28 to determne the contrbuton from the parent (p c); the equal generaton contrbuton to f and E kl determned, a before, wth the ue of Eq. 11 and 12. It hould be noted that the parent of a box account for the feld nduced by all the partcle lyng n the dtant boxe of level 1. Thu, for each level 2 box, we have now accounted for all the partcle that are outde t nearet 27 level 2 boxe. The partcle n thee 27 boxe are too cloe to an arbtrarly elected partcle n the box under conderaton and therefore we mut wat for the calculaton of the coeffcent for the fner level boxe to account for ther effect. The above procedure of combnng contrbuton from the equal generaton boxe and the parent box contnued to level 3,4,...,m lev. At all thee level, the total number of equal generaton boxe from whch the contrbuton are computed equal 189, except for the fnet m lev level, for whch we um over all the 216 boxe. Th nclude addtonal 27 nearet neghbor boxe wth one mall dfference: the ngular part 1/r removed from S 1 before computng the contrbuton from thee nearet 27 boxe. Phycally, th account for all the partcle that are lyng n the perodc mage of the nearet neghbor boxe at the fnet m lev but not the partcle n the nearet boxe themelve whch are too cloe to permt the ue of far-feld repreentaton n determnng the regular feld expanon. We hall account for thee partcle eparately va Step 4. Fnally, we compute the contrbuton to f and E kl of each partcle from the fnet level parent box. There, of coure, no contrbuton from the equal generaton boxe at the partcle level. 4 Partcle to partcle contrbuton. The contrbuton from the partcle n the nearet 27 boxe are evaluated n the ame way a for the contrbuton from the equal generaton boxe n the prevou tep except that the functon S 1 (r) now replaced by 1/r becaue the regular part of S 1 ha already been accounted for n Step 3. 5 Determne new gue for the multpole. The Step 2 4 conttute one teraton n olvng for the multpole 1996 Phy. Flud, Vol. 8, No. 8, Augut 1996 A. S. Sangan and G. Mo

10 of the partcle. A utable teratve procedure, uch a the generalzed moment redual GMRES method, ued to obtan the new gue for the multpole. Step 2 5 mut be repeated untl the multpole converge to wthn a pecfed accuracy. We now make everal remark regardng the procedure outlned above. Remark 1. For problem n upenon mechanc, we typcally ue the perodc boundary condton. For th pecal cae, creatng the herarchy tree a trval matter. Once the bac unt cell dvded nto a pecfed number of level, th tree reman unchanged throughout the dynamc mulaton. In order that th reman computatonally effcent, the number of partcle n any of the fnet level boxe mut not become much greater than t average value P. Th wll be true provded that no olated cluter wth a large number denty develop a the mulaton proceed. Th an mportant conderaton n tellar dynamc where the overall number denty of partcle tar/planet very mall and the cluter galaxy formaton an mportant phenomenon to be nvetgated through mulaton. In uch a cae, m lev may have to be changed durng the mulaton and may not reman unform throughout the bac cell. The computatonal effort for the determnaton of the tree for uch hghly nonunform ytem cale a N(logN) 4 a hown by Aluru and co-worker. 27,28 The number denty of partcle n mot upenon problem typcally large and the probablty of developng a hghly nonunform upenon generally mall. In few exceptonal cae, uch a ga old fludzed bed where large vod devod of any partcle may form, creatng tree wth nonunform m lev may prove ueful. Remark 2. If the multpole moment repreentng the effect of group of partcle are computed up to nn p, the computatonal effort for the upward pa cale a (N p 1) 4 N: there are a total of (N p 1) 2 multpole coeffcent to be evaluated and each depend lnearly on the ame number of multpole of t chldren. The computatonal cot for computng the parent to chld contrbuton to the coeffcent E kl n the regular expanon alo O((N p 1) 4 N), aumng that thee coeffcent are alo computed up to kn p. The cot of computng the contrbuton from the equal generaton boxe roughly 216/P tme that for the parent to chld calculaton, P beng the average number of partcle per box. Fnally, the partcle to partcle contrbuton requre an O(27P(N 1) 4 N) effort. Here, N the order of multpole retaned n decrbng the feld nduced by the partcle. Thu, a a frt approxmaton, the total computatonal cot per one teraton controlled by the equal generaton contrbuton and the partcle to partcle contrbuton. A rough etmate of the total operaton count therefore 216(N p 1) 4 /P27P(N 1) 4 N and th ha a mnmum for P3(N p 1)/(N 1) 2. Of coure, th to be ued only a a rough gude to etmate how optmum P mght depend on N and N p. More accurate etmate can be obtaned through numercal expermentaton. The total operaton count and the etmate of optmum P obtaned here are dfferent from that of Greengard and Rokhln 12 who ued a lghtly more complex algorthm 3 whch cale a N p ntead of the fourth power dependence obtaned n the preent algorthm. Smlar reducton n the exponent of N p obtaned n a related calculaton by Znchenko. 29 Thee nvetgator condered very hgh value of N p for whch the reducton gnfcant. A wll be hown n Sec. IV, a very good accuracy obtaned even wth N p a mall a 3 and therefore we have not mplemented ther method here. Remark 3. If the dmenon of the unt cell doe not change n dynamc mulaton, then t poble to ave conderable computatonal tme by torng varou matrce that are needed n computng the parent to chld or chld to parent contrbuton, and the contrbuton from the equal generaton boxe. In partcular, the only place where one need to ue Ewald technque for determnng S 1 and t dervatve n the equal generaton computaton and thee calculaton need to be done only once, at the begnnng of the mulaton. Alo the total number of dervatve to be evaluated O(4N 2 p logn), whch amount to a neglgble cot compared wth a total dervatve of O(4N 2 N 2 ) that one mut evaluate at every tme tep n the O(N 2 ) algorthm decrbed n the prevou ecton. III. THE METHOD FOR STOKES INTERACTIONS Havng decrbed n detal the method for Laplace nteracton, we now conder the method for Stoke nteracton. The bac dea ame a before and we need to addre only two mportant ue: how to nclude the lubrcaton effect uch that reaonably accurate partcle traectore are obtaned wth very few unknown per partcle; and how to tranlate the ngular and regular oluton of Stoke equaton. Of coure, the lubrcaton effect could alo be mportant n ome problem nvolvng Laplace nteracton, e.g., the problem of determnng the effectve thermal conductvty of dene upenon contng of hghly conductng ncluon, but we choe to defer the dcuon of the ue to the preent ecton to explan the mportant apect of the algorthm through a relatvely mple problem for whch the lubrcaton effect are abent. We hall follow the method of Sangan and Mo 8 to account for the lubrcaton force n Stoke flow. Th method eparate the force denty on the urface of the partcle nto a ngular dtrbuton of the force denty near the narrow gap between the partcle and a regular dtrbuton of force denty over the entre urface of the partcle. The ngular force denty gve aymptotcally correct force on the partcle n term of ther velocte and the gap wdth whle the regular dtrbuton expanded n the cae of phercal partcle n a ere of multpole at the center of the partcle, and ther value are determned by atfyng the boundary condton on the urface of the partcle. In addton to gvng correct lubrcaton force and torque on the partcle n cloe proxmty, the method alo account for the effect of the velocty nduced by the lubrcaton force on the other partcle n the upenon. The velocty of the flud gven by N u xu x 1 M v xx u lub x, 30 Phy. Flud, Vol. 8, No. 8, Augut 1996 A. S. Sangan and G. Mo 1997

11 where u the average velocty of the upenon, v a patally perodc Green functon for the Stoke equaton, M a dfferental operator, and u lub the velocty nduced by the lubrcaton force denty. Detaled expreon for each of thee quantte may be found n Mo and Sangan 7 and Sangan and Mo. 8 In partcular, (F /4)v (r) the velocty at r due to pont force F actng at the lattce pont of the perodc array. A hown by Hamoto, 25 v S 1 2 S 2 r r, 31 where S 1 the ame functon a ntroduced earler n the Laplace nteracton calculaton, and S 2 atfe 2 S 2 S 1. v (r) ha a ngular behavor near r0 a gven by v v 1 r r r r, 32 the well-known Oeen tenor for the flow nduced due to a pont force at orgn n a flud at ret at nfnty. The actual expreon for the dfferental operator M omewhat nvolved but, fortunately, wll not be needed for our dcuon. The only thng that we need to note that t defned uch that, when operated on v, t produce term that concde wth the ngular term n the Lamb general oluton n term of phercal harmonc. More pecfcally, let the velocty of the flud near the urface of partcle be expanded n the Lamb oluton a u u, u r, 33 wth u, and u r, beng, repectvely, the ngular and regular part of u at xx. Thee are defned by u, r n1 c n r 2 p, n b n rp, n xr, n, n, 34 where rxx, c n 2n 2n2n1, b n n1 n2n1, 35 and p n, n, and n are phercal harmonc of degree n1. For th ecton we temporarly uppre our prevou notaton accordng to whch the volume fracton of the partcle. We defne the above phercal harmonc n term of multpole coeffcent P nm, etc., by mean of p n, m, P nm n, m, T nm n, m, nm,,, r 2n1, r 2n1, r 2n1, 36 where the ummaton over m from 0 to n and for from 0 to 1. Lkewe, the regular part wrtten a u r, r n1 wth c r n c n1 p n r, m, P nm n r, m, T nm n r, m, nm c n r r 2 p n r, b n r rp n r, xr n r, n r,,, b r n b n1, and r, r,,, r, In Mo and Sangan, 7 we have defned the dfferental operator M n term of the coeffcent P, nm, etc., that appear n Eq. 36 uch that u, M v, 39 where v the Oeen tenor cf. Eq. 32. We alo gave expreon for evaluatng the coeffcent that appear n the regular part of the velocty at x n term of the ngular coeffcent P, kl, etc., of all the partcle n the upenon. Th analogou to the expreon we cted for the Laplace nteracton cf. Eq. 11 except that the correpondng expreon for the Stoke nteracton are conderably more nvolved. The drect evaluaton of thee regular coeffcent requre an O(N 2 ) computatonal effort. In the preent ecton we hall derve the reult for the tranlaton of regular and ngular oluton that wll allow u to determne the regular coeffcent wth an O(N) effort. A. Tranlaton of Stoke ngularte We wh to tranlate u c M c v (xx c ) wth t ngularte at x c to a velocty feld wth t ngularte at x p uch that both are equvalent at a pont x uffcently far away from both x c and x p. Snce the feld wth ngularte at x p mut alo be patally perodc, the mot general form for t gven by u p e M p v xx p, 40 where e a contant. Let p c and p p be the correpondng preure feld. Subttutng p for C n Eq. 14 we obtan r 2 p c dv r V r 2 p p dv r, 41 V where rxx p. Now nce the preure atfe the Laplace equaton except at t ngularte, the ntegral n the above expreon can be evaluated mply from the ngular behavor of p whch can be wrtten a p P kl k,l, Y kl r 2k1 kl k,l, 1 P kl D kl r 1, 42 where we have made ue of Eq. A1 n wrtng the lat equalty. Notng that 2 r 1 4(r), t relatvely eay to carry out ntegraton n Eq. 41 to obtan a relaton mlar to Eq Phy. Flud, Vol. 8, No. 8, Augut 1996 A. S. Sangan and G. Mo

12 P,p nm nm nm 1 kl P,c kl D kl,k,l r pc, 43 where r pc x p x c. Now we determne T,p nm. Let u be the vortcty. Ung Eq. 34 and 35, t can be hown that the ngular part of the vortcty gven by,a n 1 n ra p n,a n n,a r a 2 n,a, 44 where the upercrpt a tand for c a well a p, and r a xx a. Now we note that r a atfe the Laplace equaton at all pont except at t ngular pont x a. Th can be een by multplyng Eq. 44 wth r and ung r a rr ap to yeld r,a n 1 n rap rp n,a nn1nr ap r 2 2 r ap r 2 n. 45 Takng Laplacan of the above equaton and ung reult uch a r a n,a (n1) n,a nce n,a a homogeneou polynomal of degree n1 nr a ) and rr a r ap we obtan 2 r,a n 1 n rap r 2 p n,a n 2 5n6 n2r ap r r ap r 2 2,a n. 46 Now ubttutng r for C n Eq. 14, ung the generalzed functon repreentaton of Laplacan of p n and n, and mplfyng the reultng ntegral we obtan nn1 T,p 1 nm nm nm k,l, kl klkn1t,c D kl D kl r rrr pc. 1 k P kl,c r 47 Th can be further mplfed ung the general reult for dfferentaton of phercal harmonc gven n Appendx A. A convenent et of formula for computng all the multpole at x p from thoe at x c gven n Appendx B. To compute the coeffcent,p nm we tart wth the dentty x u u u p u, 48 x x where p (u /x u /x ) the tre tenor correpondng to a feld (u,p) and the tre correpondng to a regular feld (u,p). (u,p) on the other hand, allowed to be ngular at ome pont n the pace. We now chooe the regular feld to be gven by p r, uc r n r 2 b r n r, 49 ubttute for (u,p) both (u c,p c ) and (u p,p p ) n turn, ntegrate the dentty 48 over a volume V large enough to contan both x c and x p, apply the dvergence theorem, and ue the equvalence of the two feld at all pont on the boundary V to obtan c r n r 2 rb r n r r c r u c dv r V c r n r 2 rb r n r r p V r u p dv r. 50 Snce the dvergence of tre and velocty are zero except at the ngular pont, only the ngular part of the velocty and tre wll contrbute to the above ntegral. Subttutng the ngular part of the velocty for u a, where a tand for c or p, the ntegrand n the above expreon reduce to k 1 k c r nr 2 c r n r 2 b r n r b r n r r a c k r a 2 2 p k r a 2 k 2 k. 51 Ung the generalzed functon repreentaton of Laplacan of p k, etc., and carryng out the ntegraton n Eq. 50 we obtan,p nm nm nm kl,k,l D kl D kl D kl r r 2,c D kl 1 n1 T kl,c r pc P kl,cc r n c k kn1 1 1 kn1 k2k1r 2k r 2k 2k2k1 r2 D kl. 52 rr pc A convenent formula for evaluatng nm baed on the above expreon gven n Appendx B. Fnally, to complete the tranformaton of the ngular oluton at x c to that at x p, we need to determne the contant e n Eq. 40. For th purpoe we ue the dentty u c r u c dv u p r u p dv ru n da, 53 where the unt cell enclong both x c and x p and n a unt outward normal on t urface. A before, we have ued the equvalence of u c and u p on. Snce v and t dervatve are olenodal, and nce ther ntegral over the unt cell vanh, ubttutng for u c and u p cf. Eq. 40 yeld e0. Phy. Flud, Vol. 8, No. 8, Augut 1996 A. S. Sangan and G. Mo 1999

13 B. Tranlaton of regular oluton of Stoke equaton We now conder a oluton of Stoke equaton whch regular both at x p and x c and for whch the coeffcent (P r,p nm,t r,p nm, r,p nm ) n the regular Lamb oluton around x p are known. Our goal to derve expreon for t expanon around x c,.e., to determne the coeffcent P r,c r,c nm,t nm and r,c nm. Snce the preure atfe the Laplace equaton, the coeffcent n t expanon are related by the ame expreon a for E kl n Sec. II cf. Eq. 28 wth f 0 P r,c kl kl,n,m P nm r,p D kl r cp. 54 Smlarly, we ue the fact that r r wth rxx c atfe the Laplace equaton and obtan kk1t r,c kl kl r r r0 kl,n,m kn1t r,p nm D kl P r,c nm r D kl r rr cp. r cp 1 n1 55 Fnally, we ue the fact that r u r bharmonc, and therefore r,c kl can be evaluated from 7 r,c kl kl k D kl klkl1 4k2 2 D k2,l r u r. rr cp 56 Once agan, the detaled expreon for determnng varou coeffcent of the regular part of the velocty are gven n Appendx B. C. The O(N) algorthm for Stoke nteracton The O(N) algorthm for Stoke nteracton cont of the ame tep a outlned n Sec. II. In addton to computng the contrbuton from the ngularty at the center of partcle to the regular feld near partcle, we alo calculate the flow nduced by the lubrcaton force between each par of partcle n cloe proxmty. In Sangan and Mo, 8 we gave the expreon for the flow due to lubrcaton force n term of a force dpole ngularty tuated at the center of the gap between the partcle. The upward pa now determne the equvalent force multpole of the fnet level boxe from both the force multpole of the partcle and the lubrcaton ngularte. The remander of the upward pa calculaton n whch the multpole are evaluated for the coarer level boxe reman unaffected by the lubrcaton ngularte. In the downward pa calculaton, the contrbuton from the equal generaton boxe evaluated by the expreon gven n Mo and Sangan 7 wth the center of partcle n that tudy now replaced by the center of the equal generaton box, and the center of partcle replaced by the center of the box whoe regular coeffcent are beng evaluated. Fnally, n the partcle to partcle tep, we evaluate the contrbuton from the partcle and the lubrcaton ngularte lyng n the 27 nearet neghbor boxe. For th we need addtonal expreon for computng the contrbuton to coeffcent n the regular part of the velocty near each partcle from the ngularte tuated at the center of the partcle and the lubrcaton gap. Thee expreon are gven n Appendx B. IV. APPLICATION TO FEW SPECIFIC SUSPENSION PROBLEMS In th ecton we apply the method decrbed n the prevou two ecton to few pecfc problem wth the am of aeng the utlty of the method n tudyng ytem wth large N. Snce the computatonal effort ncreae a N 4 p, we hall be partcularly ntereted n determnng the accuracy of the method for maller N p. To valdate the analytcal reult for computng the tranlaton of ngular and regular oluton of Laplace and Stoke equaton, and to tet the accuracy of the computer program, we found t very ueful to compare the reult of the program agant O(N 2 ) program whch were extenvely teted prevouly for ther accuracy. 7,8,18,24 Snce the computatonal tme requred by thee O(N 2 ) algorthm very large, the accuracy for large N wa teted by arrangng the N partcle wthn the bac unt cell n a perodc array wth each ub-unt cell contanng N 0 partcle. Typcally, the calculaton were checked wth N 0 1, whch correpond to a truly perodc array, and wth N 0 16, the partcle wthn the ub-unt cell arranged n the latter cae n a random array. Snce n the O(N 2 ) method we compute each element of the matrx A eparately and then evaluate the product A x, the mot mportant tet of the O(N) algorthm requre the drect evaluaton of th product to match wth the correpondng product evaluated by the O(N 2 ) method for any gven x. Here, for example, for the cae of Laplace nteracton, x the vector of A, nm whle the product the vector of E kl cf. Eq. 11 plu a contant tme the vector of A, kl, wth the contant dependng on the boundary condton at the urface of the partcle. The element of the matrx A beng related to the dervatve of S 1 evaluated at xx x. Takng A, nm 1 for all n,m,, and, we evaluate the mean value of E, kl over all the partcle and t varance from the mean. For the pecal cae of a perodc array wth N 0 1, the varance mut, of coure, be zero. However, the O(N) algorthm wth fnte N p ntroduce ome fluctuaton even n the cae of a perodc array. Thee fluctuaton were found to decreae rapdly wth the ncreae n N p. The mean value for each E kl wa alo found to agree well wth that obtaned from the O(N 2 ) algorthm a we hall how n more detal below. Smlar tet were alo made for the Stoke nteracton code. A. Laplace nteracton A few typcal reult for the relatve error for the pecal cae of dffuon-controlled reacton are gven n Table I. The boundary condton on the urface of partcle for th problem yeld Eq. 7. Denotng the left-hand de lh of th equaton by r, nm we calculate two meaure of the relatve error. The frt defned by E 1 1 n eq n,m, r nm, r nm, r nm,, Phy. Flud, Vol. 8, No. 8, Augut 1996 A. S. Sangan and G. Mo

Harmonic oscillator approximation

Harmonic oscillator approximation armonc ocllator approxmaton armonc ocllator approxmaton Euaton to be olved We are fndng a mnmum of the functon under the retrcton where W P, P,..., P, Q, Q,..., Q P, P,..., P, Q, Q,..., Q lnwgner functon

More information

Introduction to Interfacial Segregation. Xiaozhe Zhang 10/02/2015

Introduction to Interfacial Segregation. Xiaozhe Zhang 10/02/2015 Introducton to Interfacal Segregaton Xaozhe Zhang 10/02/2015 Interfacal egregaton Segregaton n materal refer to the enrchment of a materal conttuent at a free urface or an nternal nterface of a materal.

More information

Chapter 6 The Effect of the GPS Systematic Errors on Deformation Parameters

Chapter 6 The Effect of the GPS Systematic Errors on Deformation Parameters Chapter 6 The Effect of the GPS Sytematc Error on Deformaton Parameter 6.. General Beutler et al., (988) dd the frt comprehenve tudy on the GPS ytematc error. Baed on a geometrc approach and aumng a unform

More information

Additional File 1 - Detailed explanation of the expression level CPD

Additional File 1 - Detailed explanation of the expression level CPD Addtonal Fle - Detaled explanaton of the expreon level CPD A mentoned n the man text, the man CPD for the uterng model cont of two ndvdual factor: P( level gen P( level gen P ( level gen 2 (.).. CPD factor

More information

Scattering of two identical particles in the center-of. of-mass frame. (b)

Scattering of two identical particles in the center-of. of-mass frame. (b) Lecture # November 5 Scatterng of two dentcal partcle Relatvtc Quantum Mechanc: The Klen-Gordon equaton Interpretaton of the Klen-Gordon equaton The Drac equaton Drac repreentaton for the matrce α and

More information

Small signal analysis

Small signal analysis Small gnal analy. ntroducton Let u conder the crcut hown n Fg., where the nonlnear retor decrbed by the equaton g v havng graphcal repreentaton hown n Fg.. ( G (t G v(t v Fg. Fg. a D current ource wherea

More information

Chapter 11. Supplemental Text Material. The method of steepest ascent can be derived as follows. Suppose that we have fit a firstorder

Chapter 11. Supplemental Text Material. The method of steepest ascent can be derived as follows. Suppose that we have fit a firstorder S-. The Method of Steepet cent Chapter. Supplemental Text Materal The method of teepet acent can be derved a follow. Suppoe that we have ft a frtorder model y = β + β x and we wh to ue th model to determne

More information

Method Of Fundamental Solutions For Modeling Electromagnetic Wave Scattering Problems

Method Of Fundamental Solutions For Modeling Electromagnetic Wave Scattering Problems Internatonal Workhop on MehFree Method 003 1 Method Of Fundamental Soluton For Modelng lectromagnetc Wave Scatterng Problem Der-Lang Young (1) and Jhh-We Ruan (1) Abtract: In th paper we attempt to contruct

More information

Improvements on Waring s Problem

Improvements on Waring s Problem Improvement on Warng Problem L An-Png Bejng, PR Chna apl@nacom Abtract By a new recurve algorthm for the auxlary equaton, n th paper, we wll gve ome mprovement for Warng problem Keyword: Warng Problem,

More information

Two-Layered Model of Blood Flow through Composite Stenosed Artery

Two-Layered Model of Blood Flow through Composite Stenosed Artery Avalable at http://pvamu.edu/aam Appl. Appl. Math. ISSN: 93-9466 Vol. 4, Iue (December 9), pp. 343 354 (Prevouly, Vol. 4, No.) Applcaton Appled Mathematc: An Internatonal Journal (AAM) Two-ayered Model

More information

The multivariate Gaussian probability density function for random vector X (X 1,,X ) T. diagonal term of, denoted

The multivariate Gaussian probability density function for random vector X (X 1,,X ) T. diagonal term of, denoted Appendx Proof of heorem he multvarate Gauan probablty denty functon for random vector X (X,,X ) px exp / / x x mean and varance equal to the th dagonal term of, denoted he margnal dtrbuton of X Gauan wth

More information

Module 5. Cables and Arches. Version 2 CE IIT, Kharagpur

Module 5. Cables and Arches. Version 2 CE IIT, Kharagpur odule 5 Cable and Arche Veron CE IIT, Kharagpur Leon 33 Two-nged Arch Veron CE IIT, Kharagpur Intructonal Objectve: After readng th chapter the tudent wll be able to 1. Compute horzontal reacton n two-hnged

More information

Two Approaches to Proving. Goldbach s Conjecture

Two Approaches to Proving. Goldbach s Conjecture Two Approache to Provng Goldbach Conecture By Bernard Farley Adved By Charle Parry May 3 rd 5 A Bref Introducton to Goldbach Conecture In 74 Goldbach made h mot famou contrbuton n mathematc wth the conecture

More information

Specification -- Assumptions of the Simple Classical Linear Regression Model (CLRM) 1. Introduction

Specification -- Assumptions of the Simple Classical Linear Regression Model (CLRM) 1. Introduction ECONOMICS 35* -- NOTE ECON 35* -- NOTE Specfcaton -- Aumpton of the Smple Clacal Lnear Regreon Model (CLRM). Introducton CLRM tand for the Clacal Lnear Regreon Model. The CLRM alo known a the tandard lnear

More information

HYDRODYNAMIC LIMIT FOR A GAS WITH CHEMICAL REACTIONS

HYDRODYNAMIC LIMIT FOR A GAS WITH CHEMICAL REACTIONS October 3, 003 8:48 WSPC/Trm Sze: 9n x 6n for Proceedng bp HYDRODYNAMIC LIMIT FOR A GAS WITH CHEMICAL REACTIONS M. BISI Dpartmento d Matematca, Unvertà d Mlano, Va Saldn 50, 0133 Mlano, Italy, E-mal: b@mat.unm.t

More information

Physics 181. Particle Systems

Physics 181. Particle Systems Physcs 181 Partcle Systems Overvew In these notes we dscuss the varables approprate to the descrpton of systems of partcles, ther defntons, ther relatons, and ther conservatons laws. We consder a system

More information

MULTIPLE REGRESSION ANALYSIS For the Case of Two Regressors

MULTIPLE REGRESSION ANALYSIS For the Case of Two Regressors MULTIPLE REGRESSION ANALYSIS For the Cae of Two Regreor In the followng note, leat-quare etmaton developed for multple regreon problem wth two eplanator varable, here called regreor (uch a n the Fat Food

More information

Pythagorean triples. Leen Noordzij.

Pythagorean triples. Leen Noordzij. Pythagorean trple. Leen Noordz Dr.l.noordz@leennoordz.nl www.leennoordz.me Content A Roadmap for generatng Pythagorean Trple.... Pythagorean Trple.... 3 Dcuon Concluon.... 5 A Roadmap for generatng Pythagorean

More information

Not at Steady State! Yes! Only if reactions occur! Yes! Ideal Gas, change in temperature or pressure. Yes! Class 15. Is the following possible?

Not at Steady State! Yes! Only if reactions occur! Yes! Ideal Gas, change in temperature or pressure. Yes! Class 15. Is the following possible? Chapter 5-6 (where we are gong) Ideal gae and lqud (today) Dente Partal preure Non-deal gae (next tme) Eqn. of tate Reduced preure and temperature Compreblty chart (z) Vapor-lqud ytem (Ch. 6) Vapor preure

More information

No! Yes! Only if reactions occur! Yes! Ideal Gas, change in temperature or pressure. Survey Results. Class 15. Is the following possible?

No! Yes! Only if reactions occur! Yes! Ideal Gas, change in temperature or pressure. Survey Results. Class 15. Is the following possible? Survey Reult Chapter 5-6 (where we are gong) % of Student 45% 40% 35% 30% 25% 20% 15% 10% 5% 0% Hour Spent on ChE 273 1-2 3-4 5-6 7-8 9-10 11+ Hour/Week 2008 2009 2010 2011 2012 2013 2014 2015 2017 F17

More information

On the SO 2 Problem in Thermal Power Plants. 2.Two-steps chemical absorption modeling

On the SO 2 Problem in Thermal Power Plants. 2.Two-steps chemical absorption modeling Internatonal Journal of Engneerng Reearch ISSN:39-689)(onlne),347-53(prnt) Volume No4, Iue No, pp : 557-56 Oct 5 On the SO Problem n Thermal Power Plant Two-tep chemcal aborpton modelng hr Boyadjev, P

More information

Team. Outline. Statistics and Art: Sampling, Response Error, Mixed Models, Missing Data, and Inference

Team. Outline. Statistics and Art: Sampling, Response Error, Mixed Models, Missing Data, and Inference Team Stattc and Art: Samplng, Repone Error, Mxed Model, Mng Data, and nference Ed Stanek Unverty of Maachuett- Amhert, USA 9/5/8 9/5/8 Outlne. Example: Doe-repone Model n Toxcology. ow to Predct Realzed

More information

Kinetic-Energy Density-Functional Theory on a Lattice

Kinetic-Energy Density-Functional Theory on a Lattice h an open acce artcle publhed under an ACS AuthorChoce Lcene, whch permt copyng and redtrbuton of the artcle or any adaptaton for non-commercal purpoe. Artcle Cte h: J. Chem. heory Comput. 08, 4, 407 4087

More information

8 Waves in Uniform Magnetized Media

8 Waves in Uniform Magnetized Media 8 Wave n Unform Magnetzed Meda 81 Suceptblte The frt order current can be wrtten j = j = q d 3 p v f 1 ( r, p, t) = ɛ 0 χ E For Maxwellan dtrbuton Y n (λ) = f 0 (v, v ) = 1 πvth exp (v V ) v th 1 πv th

More information

Open Systems: Chemical Potential and Partial Molar Quantities Chemical Potential

Open Systems: Chemical Potential and Partial Molar Quantities Chemical Potential Open Systems: Chemcal Potental and Partal Molar Quanttes Chemcal Potental For closed systems, we have derved the followng relatonshps: du = TdS pdv dh = TdS + Vdp da = SdT pdv dg = VdP SdT For open systems,

More information

CHAPTER 5 NUMERICAL EVALUATION OF DYNAMIC RESPONSE

CHAPTER 5 NUMERICAL EVALUATION OF DYNAMIC RESPONSE CHAPTER 5 NUMERICAL EVALUATION OF DYNAMIC RESPONSE Analytcal soluton s usually not possble when exctaton vares arbtrarly wth tme or f the system s nonlnear. Such problems can be solved by numercal tmesteppng

More information

CHAPTER 9 LINEAR MOMENTUM, IMPULSE AND COLLISIONS

CHAPTER 9 LINEAR MOMENTUM, IMPULSE AND COLLISIONS CHAPTER 9 LINEAR MOMENTUM, IMPULSE AND COLLISIONS 103 Phy 1 9.1 Lnear Momentum The prncple o energy conervaton can be ued to olve problem that are harder to olve jut ung Newton law. It ued to decrbe moton

More information

Variable Structure Control ~ Basics

Variable Structure Control ~ Basics Varable Structure Control ~ Bac Harry G. Kwatny Department of Mechancal Engneerng & Mechanc Drexel Unverty Outlne A prelmnary example VS ytem, ldng mode, reachng Bac of dcontnuou ytem Example: underea

More information

A NUMERICAL MODELING OF MAGNETIC FIELD PERTURBATED BY THE PRESENCE OF SCHIP S HULL

A NUMERICAL MODELING OF MAGNETIC FIELD PERTURBATED BY THE PRESENCE OF SCHIP S HULL A NUMERCAL MODELNG OF MAGNETC FELD PERTURBATED BY THE PRESENCE OF SCHP S HULL M. Dennah* Z. Abd** * Laboratory Electromagnetc Sytem EMP BP b Ben-Aknoun 606 Alger Algera ** Electronc nttute USTHB Alger

More information

Estimation of Finite Population Total under PPS Sampling in Presence of Extra Auxiliary Information

Estimation of Finite Population Total under PPS Sampling in Presence of Extra Auxiliary Information Internatonal Journal of Stattc and Analy. ISSN 2248-9959 Volume 6, Number 1 (2016), pp. 9-16 Reearch Inda Publcaton http://www.rpublcaton.com Etmaton of Fnte Populaton Total under PPS Samplng n Preence

More information

Quick Visit to Bernoulli Land

Quick Visit to Bernoulli Land Although we have een the Bernoull equaton and een t derved before, th next note how t dervaton for an uncopreble & nvcd flow. The dervaton follow that of Kuethe &Chow ot cloely (I lke t better than Anderon).

More information

Implicit Integration Henyey Method

Implicit Integration Henyey Method Implct Integraton Henyey Method In realstc stellar evoluton codes nstead of a drect ntegraton usng for example the Runge-Kutta method one employs an teratve mplct technque. Ths s because the structure

More information

One-sided finite-difference approximations suitable for use with Richardson extrapolation

One-sided finite-difference approximations suitable for use with Richardson extrapolation Journal of Computatonal Physcs 219 (2006) 13 20 Short note One-sded fnte-dfference approxmatons sutable for use wth Rchardson extrapolaton Kumar Rahul, S.N. Bhattacharyya * Department of Mechancal Engneerng,

More information

Numerical Methods for Solving Turbulent Flows by Using Parallel Technologies

Numerical Methods for Solving Turbulent Flows by Using Parallel Technologies Journal of Computer and Communcaton, 0,, -5 do:0.46/cc.0.00 Publhed Onlne February 0 (http://www.crp.org/ournal/cc) Numercal Method for Solvng urbulent Flow by Ung Parallel echnologe Albek Iakhov Department

More information

Supplementary information: Efficient mass transport by optical advection

Supplementary information: Efficient mass transport by optical advection Supplementary nformaton: Effcent ma tranport by optcal advecton Veerachart Kaorndenukul, Sergey Sukhov, and Artde Dogaru CREOL, The College of Optc and Photonc Unverty of Central lorda, 4 Central lorda

More information

Problem #1. Known: All required parameters. Schematic: Find: Depth of freezing as function of time. Strategy:

Problem #1. Known: All required parameters. Schematic: Find: Depth of freezing as function of time. Strategy: BEE 3500 013 Prelm Soluton Problem #1 Known: All requred parameter. Schematc: Fnd: Depth of freezng a functon of tme. Strategy: In thee mplfed analy for freezng tme, a wa done n cla for a lab geometry,

More information

Root Locus Techniques

Root Locus Techniques Root Locu Technque ELEC 32 Cloed-Loop Control The control nput u t ynthezed baed on the a pror knowledge of the ytem plant, the reference nput r t, and the error gnal, e t The control ytem meaure the output,

More information

Improvements on Waring s Problem

Improvements on Waring s Problem Imrovement on Warng Problem L An-Png Bejng 85, PR Chna al@nacom Abtract By a new recurve algorthm for the auxlary equaton, n th aer, we wll gve ome mrovement for Warng roblem Keyword: Warng Problem, Hardy-Lttlewood

More information

A Result on a Cyclic Polynomials

A Result on a Cyclic Polynomials Gen. Math. Note, Vol. 6, No., Feruary 05, pp. 59-65 ISSN 9-78 Copyrght ICSRS Pulcaton, 05.-cr.org Avalale free onlne at http:.geman.n A Reult on a Cyclc Polynomal S.A. Wahd Department of Mathematc & Stattc

More information

728. Mechanical and electrical elements in reduction of vibrations

728. Mechanical and electrical elements in reduction of vibrations 78. Mechancal and electrcal element n reducton of vbraton Katarzyna BIAŁAS The Slean Unverty of Technology, Faculty of Mechancal Engneerng Inttute of Engneerng Procee Automaton and Integrated Manufacturng

More information

Numerical Heat and Mass Transfer

Numerical Heat and Mass Transfer Master degree n Mechancal Engneerng Numercal Heat and Mass Transfer 06-Fnte-Dfference Method (One-dmensonal, steady state heat conducton) Fausto Arpno f.arpno@uncas.t Introducton Why we use models and

More information

NUMERICAL DIFFERENTIATION

NUMERICAL DIFFERENTIATION NUMERICAL DIFFERENTIATION 1 Introducton Dfferentaton s a method to compute the rate at whch a dependent output y changes wth respect to the change n the ndependent nput x. Ths rate of change s called the

More information

KEY POINTS FOR NUMERICAL SIMULATION OF INCLINATION OF BUILDINGS ON LIQUEFIABLE SOIL LAYERS

KEY POINTS FOR NUMERICAL SIMULATION OF INCLINATION OF BUILDINGS ON LIQUEFIABLE SOIL LAYERS KY POINTS FOR NUMRICAL SIMULATION OF INCLINATION OF BUILDINGS ON LIQUFIABL SOIL LAYRS Jn Xu 1, Xaomng Yuan, Jany Zhang 3,Fanchao Meng 1 1 Student, Dept. of Geotechncal ngneerng, Inttute of ngneerng Mechanc,

More information

Start Point and Trajectory Analysis for the Minimal Time System Design Algorithm

Start Point and Trajectory Analysis for the Minimal Time System Design Algorithm Start Pont and Trajectory Analy for the Mnmal Tme Sytem Degn Algorthm ALEXANDER ZEMLIAK, PEDRO MIRANDA Department of Phyc and Mathematc Puebla Autonomou Unverty Av San Claudo /n, Puebla, 757 MEXICO Abtract:

More information

Advanced Quantum Mechanics

Advanced Quantum Mechanics Advanced Quantum Mechancs Rajdeep Sensarma! sensarma@theory.tfr.res.n ecture #9 QM of Relatvstc Partcles Recap of ast Class Scalar Felds and orentz nvarant actons Complex Scalar Feld and Charge conjugaton

More information

MODELLING OF TRANSIENT HEAT TRANSPORT IN TWO-LAYERED CRYSTALLINE SOLID FILMS USING THE INTERVAL LATTICE BOLTZMANN METHOD

MODELLING OF TRANSIENT HEAT TRANSPORT IN TWO-LAYERED CRYSTALLINE SOLID FILMS USING THE INTERVAL LATTICE BOLTZMANN METHOD Journal o Appled Mathematc and Computatonal Mechanc 7, 6(4), 57-65 www.amcm.pcz.pl p-issn 99-9965 DOI:.75/jamcm.7.4.6 e-issn 353-588 MODELLING OF TRANSIENT HEAT TRANSPORT IN TWO-LAYERED CRYSTALLINE SOLID

More information

Modeling of Wave Behavior of Substrate Noise Coupling for Mixed-Signal IC Design

Modeling of Wave Behavior of Substrate Noise Coupling for Mixed-Signal IC Design Modelng of Wave Behavor of Subtrate Noe Couplng for Mxed-Sgnal IC Degn Georgo Veron, Y-Chang Lu, and Robert W. Dutton Center for Integrated Sytem, Stanford Unverty, Stanford, CA 9435 yorgo@gloworm.tanford.edu

More information

A particle in a state of uniform motion remain in that state of motion unless acted upon by external force.

A particle in a state of uniform motion remain in that state of motion unless acted upon by external force. The fundamental prncples of classcal mechancs were lad down by Galleo and Newton n the 16th and 17th centures. In 1686, Newton wrote the Prncpa where he gave us three laws of moton, one law of gravty,

More information

Design of Recursive Digital Filters IIR

Design of Recursive Digital Filters IIR Degn of Recurve Dgtal Flter IIR The outut from a recurve dgtal flter deend on one or more revou outut value, a well a on nut t nvolve feedbac. A recurve flter ha an nfnte mule reone (IIR). The mulve reone

More information

PHYS 705: Classical Mechanics. Newtonian Mechanics

PHYS 705: Classical Mechanics. Newtonian Mechanics 1 PHYS 705: Classcal Mechancs Newtonan Mechancs Quck Revew of Newtonan Mechancs Basc Descrpton: -An dealzed pont partcle or a system of pont partcles n an nertal reference frame [Rgd bodes (ch. 5 later)]

More information

Introduction to Vapor/Liquid Equilibrium, part 2. Raoult s Law:

Introduction to Vapor/Liquid Equilibrium, part 2. Raoult s Law: CE304, Sprng 2004 Lecture 4 Introducton to Vapor/Lqud Equlbrum, part 2 Raoult s Law: The smplest model that allows us do VLE calculatons s obtaned when we assume that the vapor phase s an deal gas, and

More information

CHAPTER 14 GENERAL PERTURBATION THEORY

CHAPTER 14 GENERAL PERTURBATION THEORY CHAPTER 4 GENERAL PERTURBATION THEORY 4 Introducton A partcle n orbt around a pont mass or a sphercally symmetrc mass dstrbuton s movng n a gravtatonal potental of the form GM / r In ths potental t moves

More information

Recursive Construction of the Bosonic Bogoliubov Vacuum State

Recursive Construction of the Bosonic Bogoliubov Vacuum State Quant. Phy. Lett. 2, No. 1, 11-15 2013 11 Quantum Phyc Letter An Internatonal Journal http://dx.do.org/10.12785/qpl/020102 Recurve Contructon of the Boonc Bogolubov Vacuum State Drceu Porte Jr 1, Marco

More information

Electromagnetic scattering. Graduate Course Electrical Engineering (Communications) 1 st Semester, Sharif University of Technology

Electromagnetic scattering. Graduate Course Electrical Engineering (Communications) 1 st Semester, Sharif University of Technology Electromagnetc catterng Graduate Coure Electrcal Engneerng (Communcaton) 1 t Semeter, 1390-1391 Sharf Unverty of Technology Content of lecture Lecture : Bac catterng parameter Formulaton of the problem

More information

MA 323 Geometric Modelling Course Notes: Day 13 Bezier Curves & Bernstein Polynomials

MA 323 Geometric Modelling Course Notes: Day 13 Bezier Curves & Bernstein Polynomials MA 323 Geometrc Modellng Course Notes: Day 13 Bezer Curves & Bernsten Polynomals Davd L. Fnn Over the past few days, we have looked at de Casteljau s algorthm for generatng a polynomal curve, and we have

More information

Physics 53. Rotational Motion 3. Sir, I have found you an argument, but I am not obliged to find you an understanding.

Physics 53. Rotational Motion 3. Sir, I have found you an argument, but I am not obliged to find you an understanding. Physcs 53 Rotatonal Moton 3 Sr, I have found you an argument, but I am not oblged to fnd you an understandng. Samuel Johnson Angular momentum Wth respect to rotatonal moton of a body, moment of nerta plays

More information

Solution Thermodynamics

Solution Thermodynamics Soluton hermodynamcs usng Wagner Notaton by Stanley. Howard Department of aterals and etallurgcal Engneerng South Dakota School of nes and echnology Rapd Cty, SD 57701 January 7, 001 Soluton hermodynamcs

More information

CHAPTER X PHASE-CHANGE PROBLEMS

CHAPTER X PHASE-CHANGE PROBLEMS Chapter X Phae-Change Problem December 3, 18 917 CHAPER X PHASE-CHANGE PROBLEMS X.1 Introducton Clacal Stefan Problem Geometry of Phae Change Problem Interface Condton X. Analytcal Soluton for Soldfcaton

More information

M. Mechee, 1,2 N. Senu, 3 F. Ismail, 3 B. Nikouravan, 4 and Z. Siri Introduction

M. Mechee, 1,2 N. Senu, 3 F. Ismail, 3 B. Nikouravan, 4 and Z. Siri Introduction Hndaw Publhng Corporaton Mathematcal Problem n Engneerng Volume 23, Artcle ID 795397, 7 page http://dx.do.org/.55/23/795397 Reearch Artcle A Three-Stage Ffth-Order Runge-Kutta Method for Drectly Solvng

More information

The influence of Stern layer conductance on the. dielectrophoretic behaviour of latex nanospheres

The influence of Stern layer conductance on the. dielectrophoretic behaviour of latex nanospheres The nfluence of Stern layer conductance on the delectrophoretc behavour of latex nanophere Mchael Pycraft Hughe* Bomedcal Engneerng Group, Unverty of Surrey, Guldford, GU2 7XH, UK Ncola Gavn Green Boelectronc

More information

Lecture Note 3. Eshelby s Inclusion II

Lecture Note 3. Eshelby s Inclusion II ME340B Elastcty of Mcroscopc Structures Stanford Unversty Wnter 004 Lecture Note 3. Eshelby s Incluson II Chrs Wenberger and We Ca c All rghts reserved January 6, 004 Contents 1 Incluson energy n an nfnte

More information

Difference Equations

Difference Equations Dfference Equatons c Jan Vrbk 1 Bascs Suppose a sequence of numbers, say a 0,a 1,a,a 3,... s defned by a certan general relatonshp between, say, three consecutve values of the sequence, e.g. a + +3a +1

More information

Extended Prigogine Theorem: Method for Universal Characterization of Complex System Evolution

Extended Prigogine Theorem: Method for Universal Characterization of Complex System Evolution Extended Prgogne Theorem: Method for Unveral Characterzaton of Complex Sytem Evoluton Sergey amenhchkov* Mocow State Unverty of M.V. Lomonoov, Phycal department, Rua, Mocow, Lennke Gory, 1/, 119991 Publhed

More information

Computer Control Systems

Computer Control Systems Computer Control ytem In th chapter we preent the element and the bac concept of computercontrolled ytem. The dcretaton and choce of amplng frequency wll be frt examned, followed by a tudy of dcrete-tme

More information

Phys 402: Raman Scattering. Spring Introduction: Brillouin and Raman spectroscopy. Raman scattering: how does it look like?

Phys 402: Raman Scattering. Spring Introduction: Brillouin and Raman spectroscopy. Raman scattering: how does it look like? Phy 402: Raman Scatterng Sprng 2008 1 Introducton: Brlloun and Raman pectrocopy Inelatc lght catterng medated by the electronc polarzablty of the medum a materal or a molecule catter rradant lght from

More information

This appendix presents the derivations and proofs omitted from the main text.

This appendix presents the derivations and proofs omitted from the main text. Onlne Appendx A Appendx: Omtted Dervaton and Proof Th appendx preent the dervaton and proof omtted from the man text A Omtted dervaton n Secton Mot of the analy provded n the man text Here, we formally

More information

Supplementary Notes for Chapter 9 Mixture Thermodynamics

Supplementary Notes for Chapter 9 Mixture Thermodynamics Supplementary Notes for Chapter 9 Mxture Thermodynamcs Key ponts Nne major topcs of Chapter 9 are revewed below: 1. Notaton and operatonal equatons for mxtures 2. PVTN EOSs for mxtures 3. General effects

More information

Plastic Analysis and Design of Steel Plate Shear Walls

Plastic Analysis and Design of Steel Plate Shear Walls 7 Platc Analy and Degn of Steel Plate Shear Wall Jeffrey Berman Department of Cvl, Structural & Envronmental Engneerng, Unverty at Buffalo Reearch Supervor: Mchel Bruneau, Profeor Summary A reved procedure

More information

Calculating Jacobian coefficients of primitive constraints with respect to Euler parameters

Calculating Jacobian coefficients of primitive constraints with respect to Euler parameters Calculatng Jacoban coeffcent of prmtve contrant wth repect to Euler parameter Yong Lu, Ha-Chuan Song, Jun-Ha Yong To cte th veron: Yong Lu, Ha-Chuan Song, Jun-Ha Yong. Calculatng Jacoban coeffcent of prmtve

More information

Supporting Information. Hydroxyl Radical Production by H 2 O 2 -Mediated. Conditions

Supporting Information. Hydroxyl Radical Production by H 2 O 2 -Mediated. Conditions Supportng Informaton Hydroxyl Radcal Producton by H 2 O 2 -Medated Oxdaton of Fe(II) Complexed by Suwannee Rver Fulvc Acd Under Crcumneutral Frehwater Condton Chrtopher J. Mller, Andrew L. Roe, T. Davd

More information

Lecture 10 Support Vector Machines II

Lecture 10 Support Vector Machines II Lecture 10 Support Vector Machnes II 22 February 2016 Taylor B. Arnold Yale Statstcs STAT 365/665 1/28 Notes: Problem 3 s posted and due ths upcomng Frday There was an early bug n the fake-test data; fxed

More information

The Price of Anarchy in a Network Pricing Game

The Price of Anarchy in a Network Pricing Game The Prce of Anarchy n a Network Prcng Game John Muaccho and Shuang Wu Abtract We analyze a game theoretc model of competng network ervce provder that trategcally prce ther ervce n the preence of elatc

More information

A NEW APPROACH IN THE RAYLEIGH - SCHRÖDINGER PERTURBATION THEORY FOR THE ROVIBRATIONAL PROBLEM

A NEW APPROACH IN THE RAYLEIGH - SCHRÖDINGER PERTURBATION THEORY FOR THE ROVIBRATIONAL PROBLEM Lebanee Scence Journal, Vol., No., A NEW APPROACH IN THE RAYLEIGH - SCHRÖDINGER PERTURBATION THEORY FOR THE ROVIBRATIONAL PROBLEM M. Korek Faculty of Scence, Berut Arab Unerty, P.O.Box - Rad El Solh, Berut

More information

Some Comments on Accelerating Convergence of Iterative Sequences Using Direct Inversion of the Iterative Subspace (DIIS)

Some Comments on Accelerating Convergence of Iterative Sequences Using Direct Inversion of the Iterative Subspace (DIIS) Some Comments on Acceleratng Convergence of Iteratve Sequences Usng Drect Inverson of the Iteratve Subspace (DIIS) C. Davd Sherrll School of Chemstry and Bochemstry Georga Insttute of Technology May 1998

More information

Physics 111. CQ1: springs. con t. Aristocrat at a fixed angle. Wednesday, 8-9 pm in NSC 118/119 Sunday, 6:30-8 pm in CCLIR 468.

Physics 111. CQ1: springs. con t. Aristocrat at a fixed angle. Wednesday, 8-9 pm in NSC 118/119 Sunday, 6:30-8 pm in CCLIR 468. c Announcement day, ober 8, 004 Ch 8: Ch 10: Work done by orce at an angle Power Rotatonal Knematc angular dplacement angular velocty angular acceleraton Wedneday, 8-9 pm n NSC 118/119 Sunday, 6:30-8 pm

More information

m = 4 n = 9 W 1 N 1 x 1 R D 4 s x i

m = 4 n = 9 W 1 N 1 x 1 R D 4 s x i GREEDY WIRE-SIZING IS LINEAR TIME Chr C. N. Chu D. F. Wong cnchu@c.utexa.edu wong@c.utexa.edu Department of Computer Scence, Unverty of Texa at Autn, Autn, T 787. ABSTRACT In nterconnect optmzaton by wre-zng,

More information

DUE: WEDS FEB 21ST 2018

DUE: WEDS FEB 21ST 2018 HOMEWORK # 1: FINITE DIFFERENCES IN ONE DIMENSION DUE: WEDS FEB 21ST 2018 1. Theory Beam bendng s a classcal engneerng analyss. The tradtonal soluton technque makes smplfyng assumptons such as a constant

More information

In this section is given an overview of the common elasticity models.

In this section is given an overview of the common elasticity models. Secton 4.1 4.1 Elastc Solds In ths secton s gven an overvew of the common elastcty models. 4.1.1 The Lnear Elastc Sold The classcal Lnear Elastc model, or Hooean model, has the followng lnear relatonshp

More information

Wind - Induced Vibration Control of Long - Span Bridges by Multiple Tuned Mass Dampers

Wind - Induced Vibration Control of Long - Span Bridges by Multiple Tuned Mass Dampers Tamkang Journal of Scence and Engneerng, Vol. 3, o., pp. -3 (000) Wnd - Induced Vbraton Control of Long - Span Brdge by Multple Tuned Ma Damper Yuh-Y Ln, Ch-Mng Cheng and Davd Sun Department of Cvl Engneerng

More information

coordinates. Then, the position vectors are described by

coordinates. Then, the position vectors are described by Revewng, what we have dscussed so far: Generalzed coordnates Any number of varables (say, n) suffcent to specfy the confguraton of the system at each nstant to tme (need not be the mnmum number). In general,

More information

The discrete dipole approximation: an overview and recent developments

The discrete dipole approximation: an overview and recent developments The dcrete dpole approxmaton: an overvew and recent development M.A. Yurkn a,b, and A.G. Hoektra a a Secton Computatonal Scence, Faculty of Scence, Unverty of Amterdam, Krulaan 40, 1098 SJ, Amterdam, The

More information

Weak McCoy Ore Extensions

Weak McCoy Ore Extensions Internatonal Mathematcal Forum, Vol. 6, 2, no. 2, 75-86 Weak McCoy Ore Extenon R. Mohammad, A. Mouav and M. Zahr Department of Pure Mathematc, Faculty of Mathematcal Scence Tarbat Modare Unverty, P.O.

More information

APPLICATIONS: CHEMICAL AND PHASE EQUILIBRIA

APPLICATIONS: CHEMICAL AND PHASE EQUILIBRIA 5.60 Sprn 2007 Lecture #28 pae PPLICTIOS: CHMICL D PHS QUILIBRI pply tattcal mechanc to develop mcrocopc model for problem you ve treated o far wth macrocopc thermodynamc 0 Product Reactant Separated atom

More information

APPROXIMATE FUZZY REASONING BASED ON INTERPOLATION IN THE VAGUE ENVIRONMENT OF THE FUZZY RULEBASE AS A PRACTICAL ALTERNATIVE OF THE CLASSICAL CRI

APPROXIMATE FUZZY REASONING BASED ON INTERPOLATION IN THE VAGUE ENVIRONMENT OF THE FUZZY RULEBASE AS A PRACTICAL ALTERNATIVE OF THE CLASSICAL CRI Kovác, Sz., Kóczy, L.T.: Approxmate Fuzzy Reaonng Baed on Interpolaton n the Vague Envronment of the Fuzzy Rulebae a a Practcal Alternatve of the Clacal CRI, Proceedng of the 7 th Internatonal Fuzzy Sytem

More information

Module 1 : The equation of continuity. Lecture 1: Equation of Continuity

Module 1 : The equation of continuity. Lecture 1: Equation of Continuity 1 Module 1 : The equaton of contnuty Lecture 1: Equaton of Contnuty 2 Advanced Heat and Mass Transfer: Modules 1. THE EQUATION OF CONTINUITY : Lectures 1-6 () () () (v) (v) Overall Mass Balance Momentum

More information

The Feynman path integral

The Feynman path integral The Feynman path ntegral Aprl 3, 205 Hesenberg and Schrödnger pctures The Schrödnger wave functon places the tme dependence of a physcal system n the state, ψ, t, where the state s a vector n Hlbert space

More information

Chapter.4 MAGNETIC CIRCUIT OF A D.C. MACHINE

Chapter.4 MAGNETIC CIRCUIT OF A D.C. MACHINE Chapter.4 MAGNETIC CIRCUIT OF A D.C. MACHINE The dfferent part of the dc machne manetc crcut / pole are yoke, pole, ar ap, armature teeth and armature core. Therefore, the ampere-turn /pole to etablh the

More information

BOUNDARY ELEMENT METHODS FOR VIBRATION PROBLEMS. Ashok D. Belegundu Professor of Mechanical Engineering Penn State University

BOUNDARY ELEMENT METHODS FOR VIBRATION PROBLEMS. Ashok D. Belegundu Professor of Mechanical Engineering Penn State University BOUNDARY ELEMENT METHODS FOR VIBRATION PROBLEMS by Aho D. Belegundu Profeor of Mechancal Engneerng Penn State Unverty ahobelegundu@yahoo.com ASEE Fello, Summer 3 Colleague at NASA Goddard: Danel S. Kaufman

More information

Chapter 7 Four-Wave Mixing phenomena

Chapter 7 Four-Wave Mixing phenomena Chapter 7 Four-Wave Mx phenomena We wll dcu n th chapter the general nonlnear optcal procee wth four nteract electromagnetc wave n a NLO medum. Frt note that FWM procee are allowed n all meda (nveron or

More information

2. SINGLE VS. MULTI POLARIZATION SAR DATA

2. SINGLE VS. MULTI POLARIZATION SAR DATA . SINGLE VS. MULTI POLARIZATION SAR DATA.1 Scatterng Coeffcent v. Scatterng Matrx In the prevou chapter of th document, we dealt wth the decrpton and the characterzaton of electromagnetc wave. A t wa hown,

More information

MATHEMATICAL AND COMPUTER HOMOGENIZATION MODELS FOR BULK MIXTURE COMPOSITE MATERIALS WITH IMPERFECT INTERFACES

MATHEMATICAL AND COMPUTER HOMOGENIZATION MODELS FOR BULK MIXTURE COMPOSITE MATERIALS WITH IMPERFECT INTERFACES Materal Phyc and Mechanc 37 (218) 34-41 Receved: December 22, 217 MATHEMATICAL AND COMPUTER HOMOGENIZATION MODELS FOR BULK MIXTURE COMPOSITE MATERIALS WITH IMPERFECT INTERFACES A.A. Naedkna 1 *, A. Rajagopal

More information

Solution Methods for Time-indexed MIP Models for Chemical Production Scheduling

Solution Methods for Time-indexed MIP Models for Chemical Production Scheduling Ian Davd Lockhart Bogle and Mchael Farweather (Edtor), Proceedng of the 22nd European Sympoum on Computer Aded Proce Engneerng, 17-2 June 212, London. 212 Elever B.V. All rght reerved. Soluton Method for

More information

9 Characteristic classes

9 Characteristic classes THEODORE VORONOV DIFFERENTIAL GEOMETRY. Sprng 2009 [under constructon] 9 Characterstc classes 9.1 The frst Chern class of a lne bundle Consder a complex vector bundle E B of rank p. We shall construct

More information

MODEL OF CEMENTING ANNULUS GAS CHANNELING BASED ON THE LATTICE BOLTZMANN THEORY

MODEL OF CEMENTING ANNULUS GAS CHANNELING BASED ON THE LATTICE BOLTZMANN THEORY Journal of Theoretcal and Appled Informaton Technology 20 th February 203. Vol. 48 No.2 2005-203 JATIT & LLS. All rght reerved. ISSN: 2-8645 www.jatt.org E-ISSN: 87-35 MODEL OF CEMENTING ANNULUS GAS CHANNELING

More information

FREQUENCY DISTRIBUTIONS Page 1 of The idea of a frequency distribution for sets of observations will be introduced,

FREQUENCY DISTRIBUTIONS Page 1 of The idea of a frequency distribution for sets of observations will be introduced, FREQUENCY DISTRIBUTIONS Page 1 of 6 I. Introducton 1. The dea of a frequency dstrbuton for sets of observatons wll be ntroduced, together wth some of the mechancs for constructng dstrbutons of data. Then

More information

A Preliminary Study on Material Utilization of Stiffened Cylindrical Shells

A Preliminary Study on Material Utilization of Stiffened Cylindrical Shells Reearch Journal of Appled Scence, Engneerng and echnology 6(5): 757-763, 03 ISSN: 040-7459; e-issn: 040-7467 Maxwell Scentfc Organzaton, 03 Submtted: December 8, 0 Accepted: February 08, 03 Publhed: Augut

More information

Problem Set 9 Solutions

Problem Set 9 Solutions Desgn and Analyss of Algorthms May 4, 2015 Massachusetts Insttute of Technology 6.046J/18.410J Profs. Erk Demane, Srn Devadas, and Nancy Lynch Problem Set 9 Solutons Problem Set 9 Solutons Ths problem

More information

You must not circulate this book in any other binding or cover and you must impose this same condition on any acquirer.

You must not circulate this book in any other binding or cover and you must impose this same condition on any acquirer. 6 Interfacal thermodynamc: Gbb equaton Luuk K. Koopal Chapter 6, Interfacal thermodynamc: Gbb equaton n Interface Scence, Second edton, 008, Wagenngen Unverty, Wagenngen, The Netherland. Avalable va: http://www.reearchgate.net/profle/luuk_koopal

More information

FEEDDBACK CONTROL OF PIEZO-LAMINATE COMPOSITE PLATE. Hafez Ave, Tehran 15914, Iran

FEEDDBACK CONTROL OF PIEZO-LAMINATE COMPOSITE PLATE. Hafez Ave, Tehran 15914, Iran ICSV14 Carn Autrala 9-12 July, 2007 FEEDDBACK CONTROL OF PIEZO-LAMINATE COMPOSITE PLATE A. Yelagh Tamjan 1, M. Abouhamze 1, R. Mrzaefar 1, A.R. Ohad 1, M.R. Elam 1 1 Department of Mechancal Engneerng,

More information

Inductance Calculation for Conductors of Arbitrary Shape

Inductance Calculation for Conductors of Arbitrary Shape CRYO/02/028 Aprl 5, 2002 Inductance Calculaton for Conductors of Arbtrary Shape L. Bottura Dstrbuton: Internal Summary In ths note we descrbe a method for the numercal calculaton of nductances among conductors

More information