This is a repository copy of Parallel-in-Space-and-Time Simulation of the Three-Dimensional, Unsteady Navier-Stokes Equations for Incompressible Flow.

Size: px
Start display at page:

Download "This is a repository copy of Parallel-in-Space-and-Time Simulation of the Three-Dimensional, Unsteady Navier-Stokes Equations for Incompressible Flow."

Transcription

1 This is a reository coy of Parallel-in-Sace-and-Time Simlation of the Three-Dimensional, Unsteady Naier-Stokes Eqations for Incomressible Flow. White Rose Research Online URL for this aer: htt://erints.whiterose.ac.k/90737/ Version: Acceted Version Proceedings Paer: Croce, R, Rrecht, D orcid.org/ and Krase, R (2014) Parallel-in-Sace-and-Time Simlation of the Three-Dimensional, Unsteady Naier-Stokes Eqations for Incomressible Flow. In: Bock, HG, Hoang, XP, Rannacher, R and Schlöder, JP, (eds.) Proceedings of the Fifth International Conference on High Performance Scientific Comting, March 5-9, 2012, Hanoi, Vietnam, Modeling, Simlation and Otimization of Comlex Processes - HPSC Fifth International Conference on High Performance Scientific Comting, Mar 2012, Hanoi, Vietnam. Modeling, Simlation and Otimization of Comlex Processes. Sringer International Pblishing, ISBN htts://doi.org/ / _2 Rese Unless indicated otherwise, flltext items are rotected by coyright with all rights resered. The coyright excetion in section 29 of the Coyright, Designs and Patents Act 1988 allows the making of a single coy solely for the rose of non-commercial research or riate stdy within the limits of fair dealing. The blisher or other rights-holder may allow frther rerodction and re-se of this ersion - refer to the White Rose Research Online record for this item. Where records identify the blisher as the coyright holder, sers can erify any secific terms of se on the blisher s website. Takedown If yo consider content in White Rose Research Online to be in breach of UK law, lease notify s by ing erints@whiterose.ac.k inclding the URL of the record and the reason for the withdrawal reqest. erints@whiterose.ac.k htts://erints.whiterose.ac.k/

2 Parallel-in-Sace-and-Time Simlation of the Three-Dimensional, Unsteady Naier-Stokes Eqations for Incomressible Flow Roberto Croce and Daniel Rrecht and Rolf Krase Abstract The Parareal arallel-in-time method is combined with satial arallelization by domain decomosition into a sace-time arallel scheme for the three-dimensional incomressible Naier-Stokes eqations. Parallelization of timesteing roides a new direction of arallelization and allows to emloy additional cores to frther seed simlations after satial arallelization has satrated. We reort on nmerical exeriments erformed on a Cray XE6, simlating a drien caity flow with and withot obstacles. Distribted memory arallelization is sed in both sace and time, featring to 2048 cores in total. It is confirmed that the sace-time-arallel method can roide seed beyond the satration of the satial domain decomosition. 1 Introdction Simlating three-dimensional flows by nmerically soling the time-deendent Naier-Stokes eqations leads to hge comtational costs. In order to obtain a reasonable time-to-soltion, massiely arallel comter systems hae to be tilized. This reqires sfficient arallelism to be identifiable in the emloyed soltion algorithms. Decomosition of the satial comtational domain is by now a standard techniqe and has roen to be extremely owerfl. Neertheless, for a fixed Roberto Croce Institte of Comtational Science, Via Gisee Bffi 13, CH-6906 Lgano, Switzerland, roberto.croce@si.ch Daniel Rrecht Institte of Comtational Science, Via Gisee Bffi 13, CH-6906 Lgano, Switzerland, daniel.rrecht@si.ch Rolf Krase Institte of Comtational Science, Via Gisee Bffi 13, CH-6906 Lgano, Switzerland, rolf.krase@si.ch 1

3 2 R. Croce, D. Rrecht, R. Krase roblem size, this aroach can only sh the time-to-soltion down to some fixed threshold, below which the comtation time for each sbdomain becomes comarable to the commnication time. While re satial arallelization can roide satisfactory rntime redction, time-critical alications may reqire larger seed and hence need additional directions of arallelism in the sed nmerical schemes. One aroach that has receied increasing attention oer recent years is arallelizing the time-steing rocedre tyically sed to sole time-deendent roblems. A olar algorithm for this is Parareal, introdced in [10] and comrehensiely analyzed in [6]. Its erformance has been inestigated for a wide range of roblems, see for examle the references in [11, 12]. A first alication to the 2D-Naier-Stokes eqations, focssing on stability and accracy withot reorting rntimes, can be fond in [5]. Some exeriments with a combined Parareal/domaindecomosition method for the two-dimensional Naier-Stokes eqations hae been condcted on to 24 rocessors in [14, 15]. While they sccessflly established the general alicability of sch a sace-time arallel aroach for the Naier-Stokes eqations, the obtained seeds were ambigos: Best seeds were achieed either with a re time-arallel or a re sace-arallel aroach, deending on the roblem size. In the resent aer, the combined Parareal/domain-decomosition sace-time arallel aroach is sed to sole a qasi-2d and a flly 3D drien caity flow roblem on a state-of-the-art HPC distribted memory architectre, sing to 2,048 cores. The caability of the aroach to redce time-to-soltion below the satration oint of a re satial arallelization is demonstrated. Also it is shown that the addition of obstacles into the comtational domain, leading to more trblent flow, leads to slower conergence of Parareal. This is likely de to the reorted stability isses for hyerbolic and conection-dominated roblems, see [4, 12]. 2 Physical Model and its discretization and arallelization The behaior of three-dimensional, incomressible Newtonian flids is described by the incomressible Naier-Stokes eqations. In dimensionless form the according momentm- and continm eqation read t + = 1 Re =0 (1) with = (,,w) being the elocity field consisting of the Cartesian elocitycomonents, being the ressre and Re the dimensionless Reynolds nmber. The Naier-Stokes soler is based on the software-ackage NaSt3DGP [2, 8] and we frther extended it by an MPI-based imlementation of Parareal [10]. In NaSt3DGP, the nsteady 3D-Naier-Stokes eqations are discretized ia standard finite olme/finite differences sing the Chorin-Temam [1, 13] rojection method

4 Sace-Time-Parallel Naier-Stokes 3 on a niform Cartesian staggered mesh for robst ressre and elocity coling. A first order forward Eler scheme is sed for time discretization and as a bilding block for Parareal, see the descrition in Second order central differences are sed for the ressre gradient and diffsion. The conectie terms are discretized with a second order TVD SMART [7] wind scheme, which is basically a bonded QUICK [9] scheme. Frthermore, comlex geometries are aroximated sing a first order cell decomosition/enmeration techniqe, on which we can imose sli as well as no-sli bondary conditions. Finally, the Poisson eqation for the ressre arising in the rojection ste is soled sing a BiCGStab [16] iteratie method. 2.1 Parallelization Both the satial as well as the temoral arallelization are imlemented for distribted-memory machines sing the MPI-library. The nderlying algorithms are described in the following Parallelization in sace ia domain decomosition We niformly decomose the discrete comtational domain Ω h into P sbdomains by first comting all factorizations of P into three comonents, i.e. P=P x P y P z, with P x,p y,p z N. Then we se or re-comted factorizations of P as argments for the following cost fnction C with resect to commnication C(P x,p y,p z )= I P x J P y + J P y K P z + I P x K P z (2) with I,J and K as the total nmber of grid-cells in x-, y- and z-direction. Finally, we aly that factorization for the domain decomosition for which C is minimal, i.e. the sace decomosition is generated in iew of the oerall srface area minimization of neighboring sbdomains. Here, P is always identical to the nmber of rocessors N sace, so that each rocessor handles one sbdomain. Since the stencil is fie grid-oints large for the conectie terms and three grid-oints for the Poisson eqation, each sbdomain needs two ghost-cell rows for the elocities and one ghost-cell row for the ressre Poisson eqation. Ths or domain decomosition method needs to commnicate the elocities once at each time-ste and the ressre once at each ressre Poisson iteration Parallelization in time with Parareal For a gien time interal[0,t], we introdce a coarse temoral mesh 0= t 0 < t 1 <...< t Nc = T (3)

5 4 R. Croce, D. Rrecht, R. Krase with a niform time-ste size t = t i+1 t i. Frther, we introdce a fine time-ste δt < t and denote by N f the total nmber of fine stes and by N c the total nmber of coarse stes, that is N c t = N f δt = T. (4) Also assme that the coarse time-ste is a mltile of the fine, so that t δt =: N r N. (5) Parareal relies on the iteratie se of two integration schemes: a fine roagator F δt that is comtationally exensie, and a coarse roagator G t that is comtationally chea. We sketch the algorithm only ery briefly here, for a more detailed descrition see for examle [10]. Denote by F(y,t n+1,t n ), G(y,t n+1,t n ) the reslt of integrating from an initial ale y at time t n to a time t n+1, sing the fine or coarse scheme, resectiely. Then, the basic iteration of Parareal reads y k+1 n+1 = G t(y k+1 n,t n+1,t n )+F δt (y k n,t n+1,t n ) G t (y k n,t n+1,t n ) (6) with ser-scrits referring to the iteration index and y n corresonding to the aroximation of the soltion at time t n. (6) conerges to a soltion y n+1 = F δt (y n,t n+1,t n ), (7) that is a soltion with the accracy of the fine soler. Here, we always erform some rescribed nmber of iterations N it. We se a forward Eler scheme for both F δt and G t and simly se a larger time-ste for the coarse roagator. Exerimenting with the combination of schemes of different and/or higher order is left for ftre work. Once the ales y k n in (6) from the reios iteration are known, the comtationally exensie calclations of the ales F δt (y k n,t n+1,t n ) can be erformed in arallel for mltile coarse interals [t n,t n+1 ]. In the re time-arallel case, the time-slices are distribted to N time cores assigned for the time-arallelization. Note that in the sace-time arallel case, the time-slices are not handled by single cores bt by mltile cores, each handling one sbdomain at the secific time, see Section The theoretically obtainable seed with Parareal is bonded by s(n ) N time N it (8) with N time denoting the nmber of rocessors in the temoral arallelization and N it the nmber of iterations, see for examle [11]. From (8) it follows that the maximm achieable arallel efficiency of the time arallelization is bonded by 1/N it. Parareal is hence considered as an additional direction of arallelization to be sed when the satial arallelization is satrated bt a frther redction of time-

6 Sace-Time-Parallel Naier-Stokes 5 sace t 0 t t t t 1 N c 2 N c 1 Nc time Fig. 1 Decomosition of the time interal [0,T] into N c time-slices. The satial mesh at each oint t i is again decomosed into P sbdomains, assigned to N sace cores. Becase the satial arallelization does not need to commnicate across time-slices, the cores from eery satial mesh are ooled into one MPI commnicator. Also, in the time arallelization, only cores handling the same sbdomain at different times hae to commnicate. Note that for readability the sketched satial mesh is 2D, althogh the simlations se a flly 3D mesh. to-soltion is reqired or desirable. Some rogress has recently been made deriing time-arallel schemes with less strict efficiency bonds [3, 11] Combined arallelization in sace and time In the combined sace-time arallel aroach as sketched in Figre 1, each coarse time interal in (6) is assigned not to a single rocessor, bt to one MPI commnicator containing N sace cores, each handling one sbdomain of the corresonding time-slice. The total nmber of cores is hence N total = N time N sace. (9) Note that the commnication in time in (6) is local in the sense that each rocessor has only to commnicate with the cores handling the same sbdomain in adjacent time-slices. Also, the satial arallelization is not commnicating across time-slices, so that for the ealation of F or G in (6), no commnication between rocessors assigned to different oints in time is reqired. We ths organize all aailable cores into two tyes of MPI commnicators: (i) Satial commnicators collect all cores belonging to the soltion at one fixed time-slice, bt handling different sbdomains. They corresond to the distribted reresentation of the soltion at one fixed time-slice. There are N time satial commnicators and each contains N sace cores. (ii) Time commnicators collect all cores dealing with the same satial sbdomain, bt at different time-slices. They are sed to erform the iteratie date in (6) of the local soltion on a satial sbdomain. There are N sace time commnicators, each ooling N time cores. No secial attention was aid to how different MPI tasks are assigned to cores. Becase of the ery different commnication attern of the sace- and time-arallelization, this can resmably hae a significant effect on the oerall erformance. More detailed inestigation of the otimal lacement of tasks is lanned for ftre stdies with the here resented code.

7 6 R. Croce, D. Rrecht, R. Krase Table 1 Simlation arameters for the qasi-2d drien caity flow (Simlation 1) and the flly 3D drien caity flow with obstacles (Simlation 2). Sim. 1 : Ω h = [0,1] [0,1] [0,0.1] Sim. 2 : Ω h = [0,1] [0,1] [0,1] Sim. 1 : N x N y N z = Sim. 2 : N x N y N z = Sim. 1 : T = 80 Sim. 2 : T = 24 Both : t = 0.01 Both : δt = Both : Re = 1000 Both : bondary = 1 Sim. 1 : N sace = 1,2,4,8 Sim. 2 : N sace = 1,...,128 Sim. 1 : N time = 4,8,16 Sim. 2 : N time = 8,16,32 Fig. 2 Arrows and color lot of the Eclidean norm of the qasi two-dimensional drien caity flow field along the center lane at three oints in time t = 0.8 and t = 8.0 and t = Nmerical Examles In the following, we inestigate the erformance of the sace-time arallel aroach for two nmerical examles. The first is the classical drien-caity roblem in a qasi-2d set. Figre 2 shows the flow in a xy-lane with z = 0.05 at times t = 0.8,8.0 and The second examle is an extension where seeral obstacles are inserted into the domain, leading to flly 3D flow. Figre 3 sketches the obstacles and the flow at T = 24. Both roblems are osed on a 3D-domain with eriodic bondary conditions in z-direction (note that x and z are the horizontal coordinates, while y is the ertical coordinate). Initially, elocity and ressre are set to zero. At the er bondary, a tangential elocity bondary = 1 is rescribed, which generates a flow inside the domain as time rogresses. No-sli bondary conditions are sed at the bottom and in the two yz-bondary lanes located at x = 0 and x = 1 as well as on the obstacles. The arameters for the two simlations are smmarized in Table 1. To assess the temoral discretization error of F δt, the soltion is comared to a reference soltion comted with F δt/10, giing a maximm error of for the fll 3D flow with obstacles. That means that once the iteration of Parareal has to redced the maximm defect between the serial and arallel soltion below this threshold, the time-arallel and time-serial soltion are of comarable accracy. We se this threshold also for the qasi-2d examle, bearing in mind that the simler strctre of the flow in this case most likely renders the estimate too conseratie. The code is rn on a Cray XE6 at the Swiss National Sercomting

8 Sace-Time-Parallel Naier-Stokes 7 Fig. 3 Arrows and color lot of the Eclidean norm of the flly three-dimensional drien caity flow field with obstacles along the center lane at time t = Max. Defect to Serial Soltion Max. Defect to Serial Soltion Max. Defect to Serial Soltion Fig. 4 Maximm difference to time-serial soltion erss nmber of Parareal iterations for the qasi 2D drien caity roblem at time t = 80.0 for N time = 4 (left), N time = 8 (middle) and N time = 16 (right). Centre, featring a total of 1496 nodes, each with two 16-core 2.1GHz AMD Interlagos CPUs and 32GB memory er node. Nodes are connected by a Gemini 3D tors interconnect and the theoretical eak erformance is 402 TFlos. 3.1 Qasi-2D Drien Caity Flow Figre 4 shows the maximm difference between the time-arallel and the timeserial soltion at the end of the simlation erss the nmber of iterations of Parareal. In all three cases, the error decreases exonentially with N it. The threshold of is reached after a single iteration, indicating that the erformance of Parareal cold robably be otimized by sing a larger t. Figre 5 shows the total seed roided by the time-serial scheme rnning F δt with only sacearallelism (black dashed line) as well as by the sace-time arallel method for different ales of N time (grey lines). All seeds are measred against the rntime of the time-serial soltion rn on a single core. The re satial arallelization reaches a maximm seed of a little oer 6 sing 8 cores. For N it = 1, the sace-time ar-

9 8 R. Croce, D. Rrecht, R. Krase Total seed Time serial =4 =8 = Total nmber of cores Total seed Time serial =4 =8 = Total nmber of cores Fig. 5 Total seed of the combined sace-time arallelization for qasi 2D drien-caity flow with N it = 1 (left) and N it = 2 (right) iterations. allel scheme reaches a seed of 14 sing 64 cores. This amonts to a seed of roghly 14/ from Parareal alone. For N it = 2 the seed is down to 8, bt still noticeably larger than the satration oint of the re sace-arallel method. Note that becase of the limited efficiency of the time arallelization, the sloes of the sace-time arallel scheme are lower for larger ales of N time. 3.2 Fll 3D Drien Caity Flow with Obstacles Figre 6 shows the maximm difference between the time-arallel and the timeserial soltion deending on the nmber of Parareal iterations for for different ales of N time. In general, as in the qasi-2d case, the error decays exonentially with the nmber of iterations, bt now, articlarly rononced for N time = 32, a small nmber of iterations has to be erformed withot large effect before the error starts to decrease. This is likely de to the increased trblence cased by the obstacles, as it is known that Parareal exhibits instabilities for adection dominated roblems or hyerbolic roblems [6, 12]. A more detailed analysis of the erformance of Parareal for trblent flow and larger Reynolds nmbers is left for ftre work. Figre 7 shows the total seed measred against the rntime of the soltion rnning F δt serially with N sace = 1. The black line shows the seed for a re satial arallelization, which scales to N sace = 16 cores and then satrates at a seed of abot 18. Adding time-arallelism can significantly increase the total seed, to abot 20 for N time = 4, abot 27 for N time = 8 and to almost 40 for N time = 16 for a fixed nmber of N it = 3 iterations (left figre). Howeer, as can be seen from Figre 6, the soltion with N = 32 is significantly less accrate. The right figre shows the total seed for a nmber of iterations adjsted so that the defect of Parareal in all cases is below 10 5 in all soltion comonents (cf. Figre 6). This illstrates that there is a sweet-sot in the nmber of concrrently treated time-slices: At some oint the otential increase in seed is offset by the additional iterations reqired.

10 Sace-Time-Parallel Naier-Stokes 9 Max. defect to time serial soltion w Max. defect to time serial soltion w Max. defect to time serial soltion w Fig. 6 Maximm difference to time-serial soltion at end of simlation erss nmber of Parareal iterations for the 3D drien caity flow with obstacles for N time = 8 (left), N time = 16 (middle), N time = 32 (right). The horizontal line indicates an error leel of Total seed Time serial =8 with 3 It. =16 with 3 It. =32 with 3 It Total nmber of cores Total seed Time serial =8 with 3 It. =16 with 3 It. =32 with 6 It Total nmber of cores Fig. 7 Total seed of the combined sace-time arallelization for 3D caity flow with obstacles for a fixed nmber of N it = 3 iterations (left) and a nmber of iterations chosen to achiee a defect below 10 5 in all soltion comonents (right). Note that the soltions in the left figre are not comarable in accracy. In the resented examle, the soltion with N = 16 is clearly more efficient than the one with N = Conclsions A sace-time arallel method, coling Parareal with satial domain decomosition, is resented and sed to sole the three-dimensional, time-deendent, incomressible Naier-Stokes eqations. Two sets are analyzed: A qasi-2d drien caity examle and an extended set, where obstacles inside the domain lead to flly 3D flow. The conergence of Parareal is inestigated and seeds of the sace-time arallel aroach are comared to seeds from a re sace-arallel scheme. It is fond that Parareal conerges ery raidly for the qasi-2d case. It also conerges in the 3D case, althogh for larger nmbers of Parareal time-slices, conergence starts to stagnate for the first few iterations, likely becase of the known stability isses of Parareal for adection dominated flows. Reslts are reorted from rns on to 128 nodes with a total of 2,048 cores on a Cray XE6, illstrating the feasibility of

11 10 R. Croce, D. Rrecht, R. Krase the aroach for state-of-the-art HPC systems. The reslts clearly demonstrate the otential of time-arallelism as an additional direction of arallelization to roide additional seed after a re satial arallelization reaches satration. While the limited arallel efficiency of Parareal in its crrent form is a drawback, we exect the scalability roerties of Parareal to direct ftre research towards modified schemes with relaxed efficiency bonds. Acknowledgements This research is fnded by the Swiss High Performance and High Prodctiity Comting initiatie HP2C. Comtational resorces were roided by the Swiss National Sercomting Centre CSCS. References 1. Chorin, A.J.: Nmerical soltion of the NaierStokes eqations. Math. Comt. 22(104), (1968) 2. Croce, R., Engel, M., Griebel, M., Klitz, M.: NaSt3DGP - a Parallel 3D Flow Soler. URL htt://wissrech.ins.ni-bonn.de/research/rojects/nast3dgp/index.htm 3. Emmett, M., Minion, M.L.: Toward an efficient arallel in time method for artial differential eqations. Comm. A. Math. and Com. Sci. 7, (2012) 4. Farhat, C., Chandesris, M.: Time-decomosed arallel time-integrators: Theory and feasibility stdies for flid, strctre, and flid-strctre alications. Int. J. Nmer. Methods Engrg. 58, (2005) 5. Fischer, P.F., Hecht, F., Maday, Y.: A arareal in time semi-imlicit aroximation of the Naier-Stokes eqations. In: R. Kornhber, et al. (eds.) Domain Decomosition Methods in Science and Engineering, Lectre Notes in Comtational Science and Engineering, ol. 40, Sringer, Berlin (2005) 6. Gander, M.J., Vandewalle, S.: Analysis of the arareal time-arallel time-integration method. SIAM J. Sci. Com. 29(2), (2007) 7. Gaskell, P., La, A.: Cratre-comensated conectie transort: SMART a new bondedness-resering transort algorithm. Int. J. Nmer. Methods Fids 8, (1988) 8. Griebel, M., Dornseifer, T., Nenhoeffer, T.: Nmerical Simlation in Flid Dynamics, a Practical Introdction. SIAM, Philadelhia (1998) 9. Leonard, B.: A stable and accrate conectie modelling rocedre based on qadratic stream interolation. Comt. Methods Al. Mech. Eng. 19, (1979) 10. Lions, J.L., Maday, Y., Trinici, G.: A arareal in time discretization of PDE s. C. R. Acad. Sci. Ser. I Math. 332, (2001) 11. Minion, M.L.: A hybrid arareal sectral deferred corrections method. Comm. A. Math. and Com. Sci. 5(2), (2010) 12. Rrecht, D., Krase, R.: Exlicit arallel-in-time integration of a linear acostic-adection system. Comters & Flids 59, (2012) 13. Temam, R.: Sr l aroximation de la soltion des eqations de Naier-Stokes ar la methode des as fractionnaires II. Arch. Rational Mech. Anal. 33, (1969) 14. Trindade, J.M.F., Pereira, J.C.F.: Parallel-in-time simlation of the nsteady Naier-Stokes eqations for incomressible flow. Int J. Nmer. Meth. Flids 45, (2004) 15. Trindade, J.M.F., Pereira, J.C.F.: Parallel-in-time simlation of two-dimensional, nsteady, incomressible laminar flows. Nm. Heat Trans., Part B 50, (2006) 16. an der Vorst, H.: BiCGStab: A fast and smoothly conerging ariant of BiCG for the soltion of nonsymmetric linear systems. SIAM J. Sci. Stat. Comt. 13, 631 (1992)

A priori error analysis for transient problems using Enhanced Velocity approach in the discrete-time setting.

A priori error analysis for transient problems using Enhanced Velocity approach in the discrete-time setting. arxiv:181.04809v1 [math.na] 1 Dec 018 A riori error analysis for transient roblems sing nhanced Velocity aroach in the discrete-time setting. Yerlan Amanbek 1, and Mary F. Wheeler 1 1 Center for Sbsrface

More information

Viscous Dissipation and Heat Absorption effect on Natural Convection Flow with Uniform Surface Temperature along a Vertical Wavy Surface

Viscous Dissipation and Heat Absorption effect on Natural Convection Flow with Uniform Surface Temperature along a Vertical Wavy Surface Aailable at htt://am.ed/aam Al. Al. Math. ISSN: 93-966 Alications and Alied Mathematics: An International Jornal (AAM) Secial Isse No. (Ma 6),. 8 8th International Mathematics Conference, March,, IUB Cams,

More information

Spatial Coupling of a Lattice Boltzmann fluid model with a Finite Difference Navier-Stokes solver

Spatial Coupling of a Lattice Boltzmann fluid model with a Finite Difference Navier-Stokes solver Satial Coling of a Lattice Boltzmann flid model with a Finite Difference Navier-Stoes solver Jonas Latt Bastien Choard Pal Albqerqe arxiv:hysics/0511243v1 [hysics.com-h] 29 Nov 2005 Agst 25, 2018 Abstract

More information

Reduction of over-determined systems of differential equations

Reduction of over-determined systems of differential equations Redction of oer-determined systems of differential eqations Maim Zaytse 1) 1, ) and Vyachesla Akkerman 1) Nclear Safety Institte, Rssian Academy of Sciences, Moscow, 115191 Rssia ) Department of Mechanical

More information

ON THE PERFORMANCE OF LOW

ON THE PERFORMANCE OF LOW Monografías Matemáticas García de Galdeano, 77 86 (6) ON THE PERFORMANCE OF LOW STORAGE ADDITIVE RUNGE-KUTTA METHODS Inmaclada Higeras and Teo Roldán Abstract. Gien a differential system that inoles terms

More information

Program Burn Algorithms Based on Detonation Shock Dynamics

Program Burn Algorithms Based on Detonation Shock Dynamics Program Brn Algorithms Based on Detonation Shock Dynamics Discrete Aroimations of Detonation Flows with Discontinos Front Models J. B. Bdzil, D. S. Stewart and T. L. Jackson DX-division, Los Alamos National

More information

A Simulation-based Spatial Decision Support System for a New Airborne Weather Data Acquisition System

A Simulation-based Spatial Decision Support System for a New Airborne Weather Data Acquisition System A Simlation-based Satial Decision Sort System for a New Airborne Weather Data Acqisition System Erol Ozan Deartment of Engineering Management Old Dominion University Norfol, VA 23529 Pal Kaffmann Deartment

More information

Discontinuous Fluctuation Distribution for Time-Dependent Problems

Discontinuous Fluctuation Distribution for Time-Dependent Problems Discontinos Flctation Distribtion for Time-Dependent Problems Matthew Hbbard School of Compting, University of Leeds, Leeds, LS2 9JT, UK meh@comp.leeds.ac.k Introdction For some years now, the flctation

More information

Existence of HCMU metrics on higher genus Riemann surfaces

Existence of HCMU metrics on higher genus Riemann surfaces Existence of HCMU metrics on higher gens Riemann srfaces October 4, 0 bstract We will generalize the reslt in [CCW05] and roe the existence of HCMU metrics on higher gens K-srfaces, i.e. Riemann srfaces

More information

Network Farthest-Point Diagrams and their Application to Feed-Link Network Extension

Network Farthest-Point Diagrams and their Application to Feed-Link Network Extension Network Farthest-Point Diagrams and their Alication to Feed-Link Network Extension Prosenjit Bose Kai Dannies Jean-Lo De Carfel Christoh Doell Carsten Grimm Anil Maheshwari Stefan Schirra Michiel Smid

More information

Pressure coefficient evaluation on the surface of the SONDA III model tested in the TTP Pilot Transonic Wind Tunnel

Pressure coefficient evaluation on the surface of the SONDA III model tested in the TTP Pilot Transonic Wind Tunnel Jornal of Physics: Conference Series OPEN ACCESS Pressre coefficient evalation on the srface of the SONDA III model tested in the TTP Pilot Transonic Wind Tnnel To cite this article: M L C C Reis et al

More information

STATIC, STAGNATION, AND DYNAMIC PRESSURES

STATIC, STAGNATION, AND DYNAMIC PRESSURES STATIC, STAGNATION, AND DYNAMIC PRESSURES Bernolli eqation is g constant In this eqation is called static ressre, becase it is the ressre that wold be measred by an instrment that is static with resect

More information

A KINEMATIC WAVE MODEL FOR EMERGENCY EVACUATION PLANNING

A KINEMATIC WAVE MODEL FOR EMERGENCY EVACUATION PLANNING A KINEMATIC WAVE MODEL FOR EMERGENCY EVACUATION PLANNING KAI-FU QIU, LIANG CHEN, ZHE WANG WEN-LONG JIN Deartment of Atomation Center for Intelligent Transortation Systems University of Science and Technology

More information

Effects of MHD Laminar Flow Between a Fixed Impermeable Disk and a Porous Rotating Disk

Effects of MHD Laminar Flow Between a Fixed Impermeable Disk and a Porous Rotating Disk Effects of MHD Laminar Flow Between a Fixed Impermeable Disk and a Poros otating Disk Hemant Poonia * * Asstt. Prof., Deptt. of Math, Stat & Physics, CCSHAU, Hisar-54.. C. Chadhary etd. Professor, Deptt.

More information

The prediction of turbulence intensities in unsteady flow

The prediction of turbulence intensities in unsteady flow University of Wollongong Research Online Faclty of Engineering and Information Sciences - Papers: Part A Faclty of Engineering and Information Sciences 24 The prediction of trblence intensities in nsteady

More information

Computations of the Shock Waves at Hypersonic Velocities Taken into Account the Chemical Reactions that Appear in the Air at High Temperatures

Computations of the Shock Waves at Hypersonic Velocities Taken into Account the Chemical Reactions that Appear in the Air at High Temperatures Comtations of the Shock Waves at Hyersonic Velocities aken into Accont the Chemical Reactions that Aear in the Air at High emeratres Mihai Leonida NICLESC*,, Maris Gabriel COJOCAR Mihai Victor PRICOP,

More information

Direct linearization method for nonlinear PDE s and the related kernel RBFs

Direct linearization method for nonlinear PDE s and the related kernel RBFs Direct linearization method for nonlinear PDE s and the related kernel BFs W. Chen Department of Informatics, Uniersity of Oslo, P.O.Box 1080, Blindern, 0316 Oslo, Norway Email: wenc@ifi.io.no Abstract

More information

FRONT TRACKING FOR A MODEL OF IMMISCIBLE GAS FLOW WITH LARGE DATA

FRONT TRACKING FOR A MODEL OF IMMISCIBLE GAS FLOW WITH LARGE DATA FONT TACKING FO A MODEL OF IMMISCIBLE GAS FLOW WITH LAGE DATA HELGE HOLDEN, NILS HENIK ISEBO, AND HILDE SANDE Abstract. In this aer we stdy front tracking for a model of one dimensional, immiscible flow

More information

EFFECT OF DIMENSIONLESS NUMBER ON NATURAL CONVECTION IN AN OPEN SQUARE CAVITY HAVING PARTIALLY HEATED SQUARE CYLINDER

EFFECT OF DIMENSIONLESS NUMBER ON NATURAL CONVECTION IN AN OPEN SQUARE CAVITY HAVING PARTIALLY HEATED SQUARE CYLINDER Proceedings of the International Conference on echanical Engineering ICE) 8- December Dhaka Bangladesh ICE-TH- EFFECT OF DIEIOE BER O TR COECTIO I OPE QRE CIT HIG PRTI HETED QRE CIDER ohammed asir ddin

More information

Chebyshev Affine Arithmetic Based Parametric Yield Prediction Under Limited Descriptions of Uncertainty

Chebyshev Affine Arithmetic Based Parametric Yield Prediction Under Limited Descriptions of Uncertainty Chebyshev Affine Arithmetic Based Parametric Yield Prediction Under Limited Descritions of Uncertainty Dr. Janet Wang ECE Deartment The University of Arizona Power Leakage Exonential rise of IC ower dissiation

More information

Computational Geosciences 2 (1998) 1, 23-36

Computational Geosciences 2 (1998) 1, 23-36 A STUDY OF THE MODELLING ERROR IN TWO OPERATOR SPLITTING ALGORITHMS FOR POROUS MEDIA FLOW K. BRUSDAL, H. K. DAHLE, K. HVISTENDAHL KARLSEN, T. MANNSETH Comptational Geosciences 2 (998), 23-36 Abstract.

More information

Numerical Model for Studying Cloud Formation Processes in the Tropics

Numerical Model for Studying Cloud Formation Processes in the Tropics Astralian Jornal of Basic and Applied Sciences, 5(2): 189-193, 211 ISSN 1991-8178 Nmerical Model for Stdying Clod Formation Processes in the Tropics Chantawan Noisri, Dsadee Skawat Department of Mathematics

More information

The analysis of scoring matrix in voting system with multiple criteria and multiple places

The analysis of scoring matrix in voting system with multiple criteria and multiple places 0 rd International Conference on Advanced Management Science IPEDR vol.9 (0) (0) IACSIT Press, Singaore The analysis of scoring matrix in voting system with mltile criteria and mltile laces Fh-Hwa Franlin

More information

Designing Parametric Cubic Curves. Prof. George Wolberg Dept. of Computer Science City College of New York

Designing Parametric Cubic Curves. Prof. George Wolberg Dept. of Computer Science City College of New York Designing Parametric Cbic Crves Prof. George Wolberg Det. of Comter Science City College of New York Objectives Introdce the tyes of crves - Interolating -Hermite - Bezier - B-Sline Analyze their erformance

More information

Multiplication Algorithms for Radix-2 RN-Codings and Two s Complement Numbers

Multiplication Algorithms for Radix-2 RN-Codings and Two s Complement Numbers Laboratoire de l Informatiqe d Parallélisme École Normale Sériere de Lyon Unité Mixte de Recherche CNRS-INRIA-ENS LYON-UCBL n o 5668 Mltilication Algorithms for Radix- RN-Codings and Two s Comlement Nmbers

More information

Control Systems of a Non-stationary Plant Based on MPC and PID Type Fuzzy Logic Controller

Control Systems of a Non-stationary Plant Based on MPC and PID Type Fuzzy Logic Controller Proceedings o the International MltiConerence o Engineers and Comter Scientists 2016 Vol I,, March 16-18, 2016, Hong Kong Control Systems o a Non-stationary Plant Based on MPC and PID Tye Fzzy Logic Controller

More information

University of Bristol

University of Bristol Uniersity of Bristol AEROGUST Workshop 27 th - 28 th April 2017, Uniersity of Lierpool Presented by Robbie Cook and Chris Wales Oeriew Theory Nonlinear strctral soler copled with nsteady aerodynamics Gst

More information

Complex Tire-Ground Interaction Simulation: Recent Developments Of An Advanced Shell Theory Based Tire Model

Complex Tire-Ground Interaction Simulation: Recent Developments Of An Advanced Shell Theory Based Tire Model . ozdog and W. W. Olson Complex Tire-Grond Interaction Simlation: ecent eelopments Of n danced Shell Theory ased Tire odel EFEECE: ozdog. and Olson W. W. Complex Tire-Grond Interaction Simlation: ecent

More information

Elements. Using ABSTRACT. 1. Introduction. Anish Bangalore, India. tioned devices. often consist packed. This offering both.

Elements. Using ABSTRACT. 1. Introduction. Anish Bangalore, India. tioned devices. often consist packed. This offering both. Jornal of Alied Mathematics and Physics,, 201, 1, 20-25 Pblished Online November 201 (htt://www.scir.org/jornal/jam) htt://dx.doi.org/10.426/jam..201.16005 A Monolithic, FEM-Based Aroach for the Coled

More information

SIMULATION OF TURBULENT FLOW AND HEAT TRANSFER OVER A BACKWARD-FACING STEP WITH RIBS TURBULATORS

SIMULATION OF TURBULENT FLOW AND HEAT TRANSFER OVER A BACKWARD-FACING STEP WITH RIBS TURBULATORS THERMAL SCIENCE, Year 011, Vol. 15, No. 1, pp. 45-55 45 SIMULATION OF TURBULENT FLOW AND HEAT TRANSFER OVER A BACKWARD-FACING STEP WITH RIBS TURBULATORS b Khdheer S. MUSHATET Mechanical Engineering Department,

More information

arxiv: v2 [math.na] 7 Sep 2016

arxiv: v2 [math.na] 7 Sep 2016 A MODIFIED IMPLEMENTATION OF MINRES TO MONITOR RESIDUAL SUBVECTOR NORMS FOR BLOCK SYSTEMS ROLAND HERZOG AND KIRK M. SOODHALTER Abstract. Saddle-oint systems, i.e., strctred linear systems with symmetric

More information

Lecture 5. Differential Analysis of Fluid Flow Navier-Stockes equation

Lecture 5. Differential Analysis of Fluid Flow Navier-Stockes equation Lectre 5 Differential Analsis of Flid Flo Naier-Stockes eqation Differential analsis of Flid Flo The aim: to rodce differential eqation describing the motion of flid in detail Flid Element Kinematics An

More information

3.1 Experimental Design

3.1 Experimental Design 3 Relay Feedback Åström and Hägglnd [1] sggest the relay feedback test to generate sstained oscillation as an alternative to the conventional continos cycling techniqe. It is very effective in determining

More information

Topological Relations in the World of Minimum Bounding Rectangles: A Study with R-trees

Topological Relations in the World of Minimum Bounding Rectangles: A Study with R-trees Toological Relations in the World of Minimm Bonding Rectangles: A Stdy with R-trees Dimitris Paadias Deartment of Comter Science and Engineering University of California, San Diego CA 0-0, USA dimitris@cs.csd.ed

More information

Chapter 6 Momentum Transfer in an External Laminar Boundary Layer

Chapter 6 Momentum Transfer in an External Laminar Boundary Layer 6. Similarit Soltions Chapter 6 Momentm Transfer in an Eternal Laminar Bondar Laer Consider a laminar incompressible bondar laer with constant properties. Assme the flow is stead and two-dimensional aligned

More information

We automate the bivariate change-of-variables technique for bivariate continuous random variables with

We automate the bivariate change-of-variables technique for bivariate continuous random variables with INFORMS Jornal on Compting Vol. 4, No., Winter 0, pp. 9 ISSN 09-9856 (print) ISSN 56-558 (online) http://dx.doi.org/0.87/ijoc.046 0 INFORMS Atomating Biariate Transformations Jeff X. Yang, John H. Drew,

More information

Numerical Simulation of Three Dimensional Flow in Water Tank of Marine Fish Larvae

Numerical Simulation of Three Dimensional Flow in Water Tank of Marine Fish Larvae Copyright c 27 ICCES ICCES, vol.4, no.1, pp.19-24, 27 Nmerical Simlation of Three Dimensional Flo in Water Tank of Marine Fish Larvae Shigeaki Shiotani 1, Atsshi Hagiara 2 and Yoshitaka Sakakra 3 Smmary

More information

A taxonomy and comparison of parallel block multi-level preconditioners for the incompressible Navier Stokes equations q

A taxonomy and comparison of parallel block multi-level preconditioners for the incompressible Navier Stokes equations q Aailable online at www.sciencedirect.com Journal of Comutational Physics 7 (008) 1790 1808 www.elseier.com/locate/jc A taxonomy and comarison of arallel block multi-leel reconditioners for the incomressible

More information

Module 4. Analysis of Statically Indeterminate Structures by the Direct Stiffness Method. Version 2 CE IIT, Kharagpur

Module 4. Analysis of Statically Indeterminate Structures by the Direct Stiffness Method. Version 2 CE IIT, Kharagpur Modle Analysis of Statically Indeterminate Strctres by the Direct Stiffness Method Version CE IIT, Kharagr Lesson The Direct Stiffness Method: Trss Analysis (Contined) Version CE IIT, Kharagr Instrctional

More information

Chapter 2 Introduction to the Stiffness (Displacement) Method. The Stiffness (Displacement) Method

Chapter 2 Introduction to the Stiffness (Displacement) Method. The Stiffness (Displacement) Method CIVL 7/87 Chater - The Stiffness Method / Chater Introdction to the Stiffness (Dislacement) Method Learning Objectives To define the stiffness matrix To derive the stiffness matrix for a sring element

More information

Open Access Stability Analysis of Internet Congestion Control Model with Compound TCP Under RED

Open Access Stability Analysis of Internet Congestion Control Model with Compound TCP Under RED Send Orders for Rerints to rerints@benthamscienceae 986 The Oen Atomation and Control Systems Jornal 205 7 986992 Oen Access Stability Analysis of Internet Congestion Control Model with Comond TCP Under

More information

Flood flow at the confluence of compound river channels

Flood flow at the confluence of compound river channels Rier Basin Management VIII 37 Flood flow at the conflence of compond rier channels T. Ishikawa 1, R. Akoh 1 & N. Arai 2 1 Department of Enironmental Science and Technology, Tokyo Institte of Technology,

More information

Error estimation and adjoint based refinement for an adjoint consistent DG discretisation of the compressible Euler equations

Error estimation and adjoint based refinement for an adjoint consistent DG discretisation of the compressible Euler equations Int. J. Comting Science and Matematics, Vol., Nos. /3/4, 007 07 Error estimation and adjoint based refinement for an adjoint consistent DG discretisation of te comressible Eler eqations R. Hartmann Institte

More information

Active Flux Schemes for Advection Diffusion

Active Flux Schemes for Advection Diffusion AIAA Aviation - Jne, Dallas, TX nd AIAA Comptational Flid Dynamics Conference AIAA - Active Fl Schemes for Advection Diffsion Hiroaki Nishikawa National Institte of Aerospace, Hampton, VA 3, USA Downloaded

More information

ON THE DEVELOPMENT OF PARAMETER-ROBUST PRECONDITIONERS AND COMMUTATOR ARGUMENTS FOR SOLVING STOKES CONTROL PROBLEMS

ON THE DEVELOPMENT OF PARAMETER-ROBUST PRECONDITIONERS AND COMMUTATOR ARGUMENTS FOR SOLVING STOKES CONTROL PROBLEMS Electronic Transactions on Numerical Analysis. Volume 44,. 53 72, 25. Coyright c 25,. ISSN 68 963. ETNA ON THE DEVELOPMENT OF PARAMETER-ROBUST PRECONDITIONERS AND COMMUTATOR ARGUMENTS FOR SOLVING STOKES

More information

OPTIMAL INTEREST RATE RULES UNDER ONE-SIDED OUTPUT AND INFLATION TARGETS. Peter J. Stemp

OPTIMAL INTEREST RATE RULES UNDER ONE-SIDED OUTPUT AND INFLATION TARGETS. Peter J. Stemp OPTIMAL INTEREST RATE RULES UNDER ONE-SIDED OUTPUT AND INFLATION TARGETS b Peter J. Stem Deartment of Economics Monash Uniersit PO Box 197, Calfield East Victoria, 3145 Astralia email: eter.stem@bseco.monash.ed.a

More information

Radiation Effects on Heat and Mass Transfer over an Exponentially Accelerated Infinite Vertical Plate with Chemical Reaction

Radiation Effects on Heat and Mass Transfer over an Exponentially Accelerated Infinite Vertical Plate with Chemical Reaction Radiation Effects on Heat and Mass Transfer over an Exponentially Accelerated Infinite Vertical Plate with Chemical Reaction A. Ahmed, M. N.Sarki, M. Ahmad Abstract In this paper the stdy of nsteady flow

More information

Kinetic derivation of a finite difference scheme for the incompressible Navier Stokes equation

Kinetic derivation of a finite difference scheme for the incompressible Navier Stokes equation deriation of a finite difference scheme for the incompressible Naier Stokes eqation Mapndi K. Banda Michael Jnk Axel Klar Abstract In the present paper the low Mach nmber limit of kinetic eqations is sed

More information

FREQUENCY DOMAIN FLUTTER SOLUTION TECHNIQUE USING COMPLEX MU-ANALYSIS

FREQUENCY DOMAIN FLUTTER SOLUTION TECHNIQUE USING COMPLEX MU-ANALYSIS 7 TH INTERNATIONAL CONGRESS O THE AERONAUTICAL SCIENCES REQUENCY DOMAIN LUTTER SOLUTION TECHNIQUE USING COMPLEX MU-ANALYSIS Yingsong G, Zhichn Yang Northwestern Polytechnical University, Xi an, P. R. China,

More information

Graphs and Networks Lecture 5. PageRank. Lecturer: Daniel A. Spielman September 20, 2007

Graphs and Networks Lecture 5. PageRank. Lecturer: Daniel A. Spielman September 20, 2007 Graphs and Networks Lectre 5 PageRank Lectrer: Daniel A. Spielman September 20, 2007 5.1 Intro to PageRank PageRank, the algorithm reportedly sed by Google, assigns a nmerical rank to eery web page. More

More information

Ocean Engineering 59 (2013) Contents lists available at SciVerse ScienceDirect. Ocean Engineering

Ocean Engineering 59 (2013) Contents lists available at SciVerse ScienceDirect. Ocean Engineering Ocean Engineering 59 (2013) 231 239 Contents lists aailable at SciVerse ScienceDirect Ocean Engineering jornal homeage: www.elseier.com/locate/oceaneng simlation of waes generated by a moing ressre field

More information

Department of Economics. Issn Discussion paper 32/09. Optimal Interest Rate Rules Under One-Sided Output and Inflation Targets *

Department of Economics. Issn Discussion paper 32/09. Optimal Interest Rate Rules Under One-Sided Output and Inflation Targets * Deartment of Economics Issn 44-549 Discssion aer 3/9 Otimal Interest Rate Rles Under One-Sided Ott and Inflation Targets * Peter J. Stem Abstract: We inestigate the deriation of otimal interest rate rles

More information

Non-Linear Squeezing Flow of Casson Fluid. between Parallel Plates

Non-Linear Squeezing Flow of Casson Fluid. between Parallel Plates International Jornal o Matematical Analsis Vol. 9 5 no. 5 - HIKAI Ltd www.m-ikari.com tt://d.doi.org/.988/ijma.5.49 Non-Linear Sqeezing Flow o Casson Flid between Parallel Plates S. Ganes C. K. Kirbasankar

More information

Uniformly best wavenumber approximations by spatial central difference operators: An initial investigation

Uniformly best wavenumber approximations by spatial central difference operators: An initial investigation Uniformly best wavenumber aroximations by satial central difference oerators: An initial investigation Vitor Linders and Jan Nordström Abstract A characterisation theorem for best uniform wavenumber aroximations

More information

A New Method for Calculating of Electric Fields Around or Inside Any Arbitrary Shape Electrode Configuration

A New Method for Calculating of Electric Fields Around or Inside Any Arbitrary Shape Electrode Configuration Proceedings of the 5th WSEAS Int. Conf. on Power Systems and Electromagnetic Compatibility, Corf, Greece, Agst 3-5, 005 (pp43-48) A New Method for Calclating of Electric Fields Arond or Inside Any Arbitrary

More information

Gravity Waves in Shear and Implications for Organized Convection

Gravity Waves in Shear and Implications for Organized Convection SEPTEMBER 2009 S T E C H M A N N A N D M A J D A 2579 Gravity Waves in Shear and Imlications for Organized Convection SAMUEL N. STECHMANN Deartment of Mathematics, and Deartment of Atmosheric and Oceanic

More information

Low-emittance tuning of storage rings using normal mode beam position monitor calibration

Low-emittance tuning of storage rings using normal mode beam position monitor calibration PHYSIAL REVIEW SPEIAL TOPIS - AELERATORS AND BEAMS 4, 784 () Low-emittance tning of storage rings sing normal mode beam position monitor calibration A. Wolski* Uniersity of Lierpool, Lierpool, United Kingdom

More information

Study on the impulsive pressure of tank oscillating by force towards multiple degrees of freedom

Study on the impulsive pressure of tank oscillating by force towards multiple degrees of freedom EPJ Web of Conferences 80, 0034 (08) EFM 07 Stdy on the implsive pressre of tank oscillating by force towards mltiple degrees of freedom Shigeyki Hibi,* The ational Defense Academy, Department of Mechanical

More information

The Real Stabilizability Radius of the Multi-Link Inverted Pendulum

The Real Stabilizability Radius of the Multi-Link Inverted Pendulum Proceedings of the 26 American Control Conference Minneapolis, Minnesota, USA, Jne 14-16, 26 WeC123 The Real Stabilizability Radis of the Mlti-Link Inerted Pendlm Simon Lam and Edward J Daison Abstract

More information

TIME ACCURATE FAST THREE-STEP WAVELET-GALERKIN METHOD FOR PARTIAL DIFFERENTIAL EQUATIONS

TIME ACCURATE FAST THREE-STEP WAVELET-GALERKIN METHOD FOR PARTIAL DIFFERENTIAL EQUATIONS International Jornal of Wavelets, Mltiresoltion and Information Processing Vol. 4, No. (26) 65 79 c World Scientific Pblishing Company TIME ACCURATE FAST THREE-STEP WAVELET-GALERKIN METHOD FOR PARTIAL

More information

COMPUTING SCIENCE. University of Newcastle upon Tyne. Behaviour-Preserving Transition Insertions in Unfolding Prefixes. V.

COMPUTING SCIENCE. University of Newcastle upon Tyne. Behaviour-Preserving Transition Insertions in Unfolding Prefixes. V. UNIVERSITY OF NEWCASTLE University of Newcastle on Tyne COMPUTING SCIENCE Behavior-Preserving Transition Insertions in Unfolding Prefixes V. Khomenko TECHNICAL REPORT SERIES No. CS-TR-952 March, 2006 TECHNICAL

More information

Similarity Solution for MHD Flow of Non-Newtonian Fluids

Similarity Solution for MHD Flow of Non-Newtonian Fluids P P P P IJISET - International Jornal of Innovative Science, Engineering & Technology, Vol. Isse 6, Jne 06 ISSN (Online) 48 7968 Impact Factor (05) - 4. Similarity Soltion for MHD Flow of Non-Newtonian

More information

DELFT UNIVERSITY OF TECHNOLOGY

DELFT UNIVERSITY OF TECHNOLOGY DELFT UNIVERSITY OF TECHNOLOGY REPORT 02-01 The Krylov accelerated SIMPLER method for incompressible flow C. Vik and A. Saghir ISSN 1389-6520 Reports of the Department of Applied Mathematical Analysis

More information

A Monolithic Geometric Multigrid Solver for Fluid-Structure Interactions in ALE formulation

A Monolithic Geometric Multigrid Solver for Fluid-Structure Interactions in ALE formulation Pblished in International Jornal for nmerical Methods in Engineering, Vol 104, Isse 5, pp. 382-390, 2015 A Monolithic Geometric Mltigrid Soler for Flid-Strctre Interactions in ALE formlation Thomas Richter

More information

Turbulence and boundary layers

Turbulence and boundary layers Trblence and bondary layers Weather and trblence Big whorls hae little whorls which feed on the elocity; and little whorls hae lesser whorls and so on to iscosity Lewis Fry Richardson Momentm eqations

More information

Evaluation of de ections of the vertical on the sphere and the plane: a comparison of FFT techniques

Evaluation of de ections of the vertical on the sphere and the plane: a comparison of FFT techniques Jornal of Geodesy (1997) 71: 461±468 Evalation of de ections of the vertical on the shere and the lane: a comarison of FFT techniqes Q. W. Li 1, Y. Cai Li, Michael G. Sideris 1 Institte of Geodesy and

More information

A manufacturing network design model based on processor and worker capabilities

A manufacturing network design model based on processor and worker capabilities A manfactring network design model based on rocessor and worker caabilities Marc Paqet, Alain Martel and Benoit Montreil Aril 2005 Working Paer DT-2005-AM-1 (Revised March 2006) Network Organization Technology

More information

Numerical Simulation of Density Currents over a Slope under the Condition of Cooling Period in Lake Biwa

Numerical Simulation of Density Currents over a Slope under the Condition of Cooling Period in Lake Biwa Nmerical Simlation of Densit Crrents oer a Slope nder the Condition of Cooling Period in Lake Bia Takashi Hosoda Professor, Department of Urban Management, Koto Uniersit, C1-3-65, Kotodai-Katsra, Nishiko-k,

More information

Transient Approach to Radiative Heat Transfer Free Convection Flow with Ramped Wall Temperature

Transient Approach to Radiative Heat Transfer Free Convection Flow with Ramped Wall Temperature Jornal of Applied Flid Mechanics, Vol. 5, No., pp. 9-1, 1. Available online at www.jafmonline.net, ISSN 175-57, EISSN 175-645. Transient Approach to Radiative Heat Transfer Free Convection Flow with Ramped

More information

The Open Civil Engineering Journal

The Open Civil Engineering Journal Send Orders for Reprints to reprints@benthamscience.ae 564 The Open Ciil Engineering Jornal, 16, 1, 564-57 The Open Ciil Engineering Jornal Content list aailable at: www.benthamopen.com/tociej/ DOI: 1.174/187414951611564

More information

Fluid Dynamics. Type of Flows Continuity Equation Bernoulli Equation Steady Flow Energy Equation Applications of Bernoulli Equation

Fluid Dynamics. Type of Flows Continuity Equation Bernoulli Equation Steady Flow Energy Equation Applications of Bernoulli Equation Tye of Flows Continity Eqation Bernolli Eqation Steady Flow Energy Eqation Alications of Bernolli Eqation Flid Dynamics Streamlines Lines having the direction of the flid velocity Flids cannot cross a

More information

Hermite subdivision on manifolds via parallel transport

Hermite subdivision on manifolds via parallel transport Adances in Comutational Mathematics manuscrit No. (will be inserted by the editor Hermite subdiision on manifolds ia arallel transort Caroline Moosmüller Receied: date / Acceted: date Abstract We roose

More information

5. PRESSURE AND VELOCITY SPRING Each component of momentum satisfies its own scalar-transport equation. For one cell:

5. PRESSURE AND VELOCITY SPRING Each component of momentum satisfies its own scalar-transport equation. For one cell: 5. PRESSURE AND VELOCITY SPRING 2019 5.1 The momentum equation 5.2 Pressure-velocity couling 5.3 Pressure-correction methods Summary References Examles 5.1 The Momentum Equation Each comonent of momentum

More information

Lecture Notes: Finite Element Analysis, J.E. Akin, Rice University

Lecture Notes: Finite Element Analysis, J.E. Akin, Rice University 9. TRUSS ANALYSIS... 1 9.1 PLANAR TRUSS... 1 9. SPACE TRUSS... 11 9.3 SUMMARY... 1 9.4 EXERCISES... 15 9. Trss analysis 9.1 Planar trss: The differential eqation for the eqilibrim of an elastic bar (above)

More information

Constrained tri-connected planar straight line graphs

Constrained tri-connected planar straight line graphs Constrained tri-connected lanar straight line grahs Marwan Al-Jbeh Gill Bareet Mashhood Ishae Diane L. Soaine Csaba D. Tóth Andrew Winslow Abstract It is known that for any set V of n 4 oints in the lane,

More information

An optimizing reduced order FDS for the tropical Pacific Ocean reduced gravity model

An optimizing reduced order FDS for the tropical Pacific Ocean reduced gravity model An optimizing redced order FDS for the tropical Pacific Ocean redced gravity model Zhendong Lo a,, Jing Chen b,, Jiang Zh c,, Riwen Wang c,, and I. M. Navon d,, a School of Science, Beijing Jiaotong University,

More information

Preconditioning techniques for Newton s method for the incompressible Navier Stokes equations

Preconditioning techniques for Newton s method for the incompressible Navier Stokes equations Preconditioning techniques for Newton s method for the incomressible Navier Stokes equations H. C. ELMAN 1, D. LOGHIN 2 and A. J. WATHEN 3 1 Deartment of Comuter Science, University of Maryland, College

More information

arxiv: v1 [physics.flu-dyn] 4 Sep 2013

arxiv: v1 [physics.flu-dyn] 4 Sep 2013 THE THREE-DIMENSIONAL JUMP CONDITIONS FOR THE STOKES EQUATIONS WITH DISCONTINUOUS VISCOSITY, SINGULAR FORCES, AND AN INCOMPRESSIBLE INTERFACE PRERNA GERA AND DAVID SALAC arxiv:1309.1728v1 physics.fl-dyn]

More information

By Dr. Salah Salman. Problem (1)

By Dr. Salah Salman. Problem (1) Chemical Eng. De. Problem ( Solved Problems Samles in Flid Flow 0 A late of size 60 cm x 60 cm slides over a lane inclined to the horizontal at an angle of 0. It is searated from the lane with a film of

More information

4 Exact laminar boundary layer solutions

4 Exact laminar boundary layer solutions 4 Eact laminar bondary layer soltions 4.1 Bondary layer on a flat plate (Blasis 1908 In Sec. 3, we derived the bondary layer eqations for 2D incompressible flow of constant viscosity past a weakly crved

More information

Kragujevac J. Sci. 34 (2012) UDC 532.5: :537.63

Kragujevac J. Sci. 34 (2012) UDC 532.5: :537.63 5 Kragjevac J. Sci. 34 () 5-. UDC 53.5: 536.4:537.63 UNSTEADY MHD FLOW AND HEAT TRANSFER BETWEEN PARALLEL POROUS PLATES WITH EXPONENTIAL DECAYING PRESSURE GRADIENT Hazem A. Attia and Mostafa A. M. Abdeen

More information

MODELLING OF TURBULENT ENERGY FLUX IN CANONICAL SHOCK-TURBULENCE INTERACTION

MODELLING OF TURBULENT ENERGY FLUX IN CANONICAL SHOCK-TURBULENCE INTERACTION MODELLING OF TURBULENT ENERGY FLUX IN CANONICAL SHOCK-TURBULENCE INTERACTION Rssell Qadros, Krishnend Sinha Department of Aerospace Engineering Indian Institte of Technology Bombay Mmbai, India 476 Johan

More information

A NONLINEAR VISCOELASTIC MOONEY-RIVLIN THIN WALL MODEL FOR UNSTEADY FLOW IN STENOTIC ARTERIES. Xuewen Chen. A Thesis. Submitted to the Faculty.

A NONLINEAR VISCOELASTIC MOONEY-RIVLIN THIN WALL MODEL FOR UNSTEADY FLOW IN STENOTIC ARTERIES. Xuewen Chen. A Thesis. Submitted to the Faculty. A NONLINEAR VISCOELASTIC MOONEY-RIVLIN THIN WALL MODEL FOR UNSTEADY FLOW IN STENOTIC ARTERIES by Xewen Chen A Thesis Sbmitted to the Faclty of the WORCESTER POLYTECHNIC INSTITUTE in partial flfillment

More information

An experimental analysis of canopy flows

An experimental analysis of canopy flows Jornal of Physics: Conference Series An experimental analysis of canopy flows To cite this article: Antonio Segalini et al 11 J. Phys.: Conf. Ser. 318 718 View the article online for pdates and enhancements.

More information

Centrum voor Wiskunde en Informatica

Centrum voor Wiskunde en Informatica Centrm voor Wisknde en Informatica Probability, Networks and Algorithms Probability, Networks and Algorithms Some remarks on roerties of generalized Pickands constants K.G. Debicki, REPOR PNA-R4 FEBRUARY,

More information

Numerical issues in modeling combustion instability by quasi-1d Euler equations

Numerical issues in modeling combustion instability by quasi-1d Euler equations Original Research Article Nmerical isses in modeling combstion instability by qasi-d Eler eqations International Jornal of Sray and Combstion Dynamics 7, Vol. 9(4) 349 366! The Athor(s) 7 Rerints and ermissions:

More information

Eigenanalysis of Finite Element 3D Flow Models by Parallel Jacobi Davidson

Eigenanalysis of Finite Element 3D Flow Models by Parallel Jacobi Davidson Eigenanalysis of Finite Element 3D Flow Models by Parallel Jacobi Davidson Luca Bergamaschi 1, Angeles Martinez 1, Giorgio Pini 1, and Flavio Sartoretto 2 1 Diartimento di Metodi e Modelli Matematici er

More information

Large Eddy Simulation Of Flow Past A Two-dimensional Hill

Large Eddy Simulation Of Flow Past A Two-dimensional Hill Large Eddy Simlation Of Flow Past A Two-dimensional Hill Sankara N.Vengadesan ) and Akihiko Nakayama ) ) Research Associate, Email: vengades@kobe-.ac.jp, ) Professor, Email: nakayama@kobe-.ac.jp Gradate

More information

Lewis number and curvature effects on sound generation by premixed flame annihilation

Lewis number and curvature effects on sound generation by premixed flame annihilation Center for Trblence Research Proceedings of the Smmer Program 2 28 Lewis nmber and crvatre effects on sond generation by premixed flame annihilation By M. Talei, M. J. Brear AND E. R. Hawkes A nmerical

More information

Principles of Computed Tomography (CT)

Principles of Computed Tomography (CT) Page 298 Princiles of Comuted Tomograhy (CT) The theoretical foundation of CT dates back to Johann Radon, a mathematician from Vienna who derived a method in 1907 for rojecting a 2-D object along arallel

More information

NUMERICAL AND THEORETICAL INVESTIGATIONS ON DETONATION- INERT CONFINEMENT INTERACTIONS

NUMERICAL AND THEORETICAL INVESTIGATIONS ON DETONATION- INERT CONFINEMENT INTERACTIONS NUMERICAL AND THEORETICAL INVESTIGATIONS ON DETONATION- INERT CONFINEMENT INTERACTIONS Tariq D. Aslam and John B. Bdzil Los Alamos National Laboratory Los Alamos, NM 87545 hone: 1-55-667-1367, fax: 1-55-667-6372

More information

), σ is a parameter, is the Euclidean norm in R d.

), σ is a parameter, is the Euclidean norm in R d. WEIGHTED GRAPH LAPLACIAN AND IMAGE INPAINTING ZUOQIANG SHI, STANLEY OSHER, AND WEI ZHU Abstract. Inspired by the graph Laplacian and the point integral method, we introdce a novel weighted graph Laplacian

More information

1 JAXA Special Pblication JAXA-SP-1-E Small-scale trblence affects flow fields arond a blff body and therefore it governs characteristics of cross-sec

1 JAXA Special Pblication JAXA-SP-1-E Small-scale trblence affects flow fields arond a blff body and therefore it governs characteristics of cross-sec First International Symposim on Fltter and its Application, 1 11 IEXPERIMENTAL STUDY ON TURBULENCE PARTIAL SIMULATION FOR BLUFF BODY Hiroshi Katschi +1 and Hitoshi Yamada + +1 Yokohama National University,

More information

Sareban: Evaluation of Three Common Algorithms for Structure Active Control

Sareban: Evaluation of Three Common Algorithms for Structure Active Control Engineering, Technology & Applied Science Research Vol. 7, No. 3, 2017, 1638-1646 1638 Evalation of Three Common Algorithms for Strctre Active Control Mohammad Sareban Department of Civil Engineering Shahrood

More information

DEVELOPMENT OF A BRANCH AND PRICE APPROACH INVOLVING VERTEX CLONING TO SOLVE THE MAXIMUM WEIGHTED INDEPENDENT SET PROBLEM

DEVELOPMENT OF A BRANCH AND PRICE APPROACH INVOLVING VERTEX CLONING TO SOLVE THE MAXIMUM WEIGHTED INDEPENDENT SET PROBLEM DEVELOPMENT OF A BRANCH AND PRICE APPROACH INVOLVING VERTEX CLONING TO SOLVE THE MAXIMUM WEIGHTED INDEPENDENT SET PROBLEM A Thesis by SANDEEP SACHDEVA Submitted to the Office of Graduate Studies of Texas

More information

Suyeon Shin* and Woonjae Hwang**

Suyeon Shin* and Woonjae Hwang** JOURNAL OF THE CHUNGCHEONG MATHEMATICAL SOCIETY Volme 5, No. 3, Agst THE NUMERICAL SOLUTION OF SHALLOW WATER EQUATION BY MOVING MESH METHODS Syeon Sin* and Woonjae Hwang** Abstract. Tis paper presents

More information

BOUNDARY LAYER FLOW OF A VISCOELASTIC LIQUID NEAR A STAGNATION POINT WITH SLIP

BOUNDARY LAYER FLOW OF A VISCOELASTIC LIQUID NEAR A STAGNATION POINT WITH SLIP BOUNDARY LAYER FLOW OF A VISCOELASTIC LIQUID NEAR A STAGNATION POINT WITH SLIP ACSahoo, TBiswal Det of Mathematics, TemleCit Institte of Technolog & Engineering (TITE), F/, IID Center, Barnei, Khrda Odisha

More information

System identification of buildings equipped with closed-loop control devices

System identification of buildings equipped with closed-loop control devices System identification of bildings eqipped with closed-loop control devices Akira Mita a, Masako Kamibayashi b a Keio University, 3-14-1 Hiyoshi, Kohok-k, Yokohama 223-8522, Japan b East Japan Railway Company

More information

Estimation of Lateral Displacements for Offshore Monopiles in Clays based on CPT Results

Estimation of Lateral Displacements for Offshore Monopiles in Clays based on CPT Results Estimation of Lateral Dislacements for Offshore Monoiles in Clas based on CPT Reslts *Garam Kim 1), Jinoh Kim 2), Incheol Kim 3), Dongho Kim 4), Bngkwon Bn 5), Yanghoon Roh 6), Ohchang Kwon 7) and Jnhwan

More information

The spreading residue harmonic balance method for nonlinear vibration of an electrostatically actuated microbeam

The spreading residue harmonic balance method for nonlinear vibration of an electrostatically actuated microbeam J.L. Pan W.Y. Zh Nonlinear Sci. Lett. Vol.8 No. pp.- September The spreading reside harmonic balance method for nonlinear vibration of an electrostatically actated microbeam J. L. Pan W. Y. Zh * College

More information