An Experimental Study for Mixed Convection through a Circular Tube Filled with Porous Media and Fixed Horizontally and Inclined
|
|
- Benedict Robertson
- 5 years ago
- Views:
Transcription
1 Mdern Applied Science Vl., N. ; April 0 An Experimental Study fr Mixed Cnvectin thrugh a Circular Tube Filled with Pru Media and Fixed Hrizntally and Inclined Taheen Ahmad Taheen Mechanical Engineering, Cllege f Engineering, Tikrit Univerity, Iraq Received: December, 0 Accepted: December 17, 0 di:./ma.vnp1 Abtract The pru media have a great influence n the heat tranfer and traging it characteritic. In thi tudy an experimental wrk ha been cnducted t meaure the mixed cnvectin thugh the filled circular tube. Firt, the tet apparatu ha been manufactured; filled circular tube with a pru media and fixed hrizntally firt then tilted with different angle. Secndly, the circular tube i heated with a cntant heat flux and, thermcuple have been tickled in prper pitin. Then many reading, fr temperature, have been regitered fr each thermcuple with different peed f the utlet air (frm the circular tube) and the inclinatin angle f the tube ha been changed many time t be 0, 0,4 &. Thee experiment have been cnducted fr the range (.4 Ra 7.7) f Rayleigh number and fr the range (.1 1.4) f clet number. Three tet fr the heat flux have been cnducted, fr each five clet number ha been ued. Finally, the experimental reult hw that the urface temperature f pipe ha a prprtinal relatin with the tube length fr all value f the heat flux and clet number. In additin, the heat tranfer i achieved by free cnvectin fr mall clet number, by frced cnvectin fr large clet number and by mixed cnvectin fr medium value f clet number. Keywrd: Mixed cnvectin, Cntant heat flux, Pru media, Inclined Hrizntal circular tube Nmenclature A tube urface area (m ) C pecific heat (J.kg -1. K -1 ) D tube diameter (m) d grain diameter (m) g acceleratin due t gravity (m/ ) Gr Grahf number h heat tranfer cefficient (W.m -. C -1 ) I electrical current (ampere) K permeability (m ) k thermal cnductivity (W.m -1. C -1 ) L tube length (m) m ma flw rate (kg. -1 ) Nu Nuelt number clet number Ra Rayleigh number Re Reynld number Ri Richardn number Q heat input (W) q heat flux (W. m - ) T temperature ( C) u velcity f air (m. -1 ) 1 ISSN E-ISSN 1-1
2 Mdern Applied Science Vl., N. ; April 0 V heater vltage (vlt) Greek ymbl tube angle f inclinatin Prity kinematic vicity ( m. -1 ) dynamic vicity (kg.m ) denity (kg.m - ) percentage f heat l Subcript av average b bulk e effective f fluid (air) i inlet utlet urface p grain (gla phere) z lcal 1. Intrductin Over the lat three decade Heat tranfer thugh pru media ha received cniderable attentin in many ther field earching fr alternative energy. The analytical treatment fr cnvective heat tranfer thrugh pru lk fr the firt time cmplicated. Depending n the fluid prpertie, the temperature will effect the fluid flw in the internal and external flw and will cmplicate the aumptin f heat tranfer particularly laminar flw at lw Reynld number, the effect f the buncy can t be neglected and free cnvectin cnvicted by frced cnvectin in heat tranfer will caue a new field fr tudy called mixed cnvectin. It i difficult t knw it whle nature(dnald A. Nield and Adrian Bejan, 1)( Al- Daher M.. 000). The cmbined frced and free cnvectin in an inclined urface and aturated in a pru medium, in the cae f tream line and urface temperature ditributin will be in harmnic with ditance. The parameter (Gr/Re) i the ne wh will decide the type f the effective cnvectin, when it value i very mall the frced cnvectin i the dminant, and when it value very large the free cnvectin i dminant(ping Cheng, 00). Analytical tudy and invetigating the influence f permeability f the cmbined frce and free cnvectin arund inclined buried urface in aturated pru media wa preented by (chandraeekhara& P.M. S, 1). The reearcher had tudied tw cae, unifrm urface temperature and linearly variable with ditance meaured frm the frnt edge f the plate with aitance and pping flw. They fund that the nn-dimeninle parameter (Gr/Re ) and ( /Re) will cnduct the flw behavir, al they nticed that the permeability change will increae heat tranfer fr all ( /Re) value. (W.L etal. 1) cnducted an experiment n a mixed cnvectin heat tranfer in a vertical packed channel with a ymmetric heating f pping wall. The experiment were carried ut in the range f <<00 and 0<Ra<. The meaured temperature ditributin indicate the exitence f a ecndary cnvective cell inide the vertical packed channel. A crrelatin equatin fr Nuelt number in term f clet and Rayleigh number wa btained frm experimental data and plt the relatin between them. Three cnvectin regime were exit: frced cnvectin Ra/<1, mixed cnvectin <Ra/< and natural cnvectin </. Mixed cnvectin analyi n a vertical packed plane in tw directin uing unbalanced heat wa tudied by (Nawaf,004). He aumed ne ide i inulated and the ther ne i cled by a cntant temperature media. The tudy wa carried ut fr (0.1- ), Ra (, 0, ), thermal cnductivity rati Kr (0.01- ) and heat tranfer cefficient H (0.01- ). He fund that the net average Nuelt number decreae a H increae at lw clet number, while fr large clet number and H value and when Kr increae the average Nuelt number will increae. Publihed by Canadian Center f Science and Educatin 1
3 Mdern Applied Science Vl., N. ; April 0 (Y.M.F. etal. 00) Studied laminar mixed cnvectin in the entrance regin fr hrizntal emicircular duct with the flat wall at the bttm. They ued mmentum and energy equatin which were lved by cntrl vlume apprach uing finite cntrl vlume by SIMPLER Algrithm. Reult were fr the thermal bundary cnditin f unifrm axially heat flux and with unifrm wall temperature circumferentially t ditribute velcitie temperature and lcal Nuelt number hwed that Nu decreae in mixed cnvectin cae in the entrance regin, and decreae when the entrance length i increaed and increaed with the natural cnvectin effect befre reaching a cntant value (fully develped). While Gr and Nu increae with increaing mean cefficient f frictin fr the wall in fully develped cae. Mixed cnvectin wa tudied experimentally in a circular inclined channel with different angle and vertical fr laminar dwnward flw by (Huein, et al. 007). The ued a cpper pipe (length 0mm) inner diameter (0mm). The uter urface wa heated at cntant heat flux, Re range wa (0- ), Ra (1.7* -.* ). They fund the tune urface temperature increae a lng the tube with dwnward flw extenively increaing cmparing with upward flw. Nu in the dwnward flw i le in the upward cae. A crrelatin wa btained between Nu, Ra and Re in the till and vertical cae in the frm Nu Ra Re.. Experimental Wrk Mixed cnvectin heat tranfer i ne f the mt imprtant cnvectin tranfer we cnduct an experiment mixed cnvectin in a packed aturated pru media heated with a cntant heat flux in the hrizntal pitin and changing the inclinatin tube angle (0, 4, ) repectively. A cpper tube i ued, it internal and external diameter are (4mm) and (47mm) repectively, the length wa (0mm). The active heated length i nly (00mm). The channel wa packed with gla phere, their diameter i (mm) and their thermal cnductivity i (0.1W/m. C). They were fitted between tw permeable dic made f galvanized irn. The tube i prvided with air by a blwer at (00 rpm) and A.V at (0 v). The vltage wa tabilized by a tabilizer. The tube urface temperature wa meaured by (4) thermcuple (T type) were pitin a lng the tet ectin tube, three thermcuple were pitin fr each lcate. The mean read wa ued, thi pitin repreent ne frm 1. One thermcuple i ued t meaure the air temperature at the entrance f the tube which wa lcated in the air flw, anther ne wa lcated after packed t meaure the ut flw air temperature and it wa pitined in the ame perviu way. Anther thermcuple meaure the labratry ambient temperature. The tet ectin wa heated electrically uing cil and an electrical reitance arund tube f (m) in length with a reitance (1 /m). T increae the upplied pwer the tet ectin wa thermally inulated with fiber gla f (mm) in thickne. The tw end f the tube were inulated electrically and thermally uing tw part f tephln made f inulatr and thermal reitr lapanate al it wa ued t reduce the thermal le in the axial directin. The entrance ectr wa packed t be inure t get fully develped befre the tet ectin. The heater wa upplied with an alternative electrical pwer uing cnverter that upplied with a teady vltage thrugh a vltage regulatr (0v). An Ameter wa ued t meaure the current pa thrugh the heater with accuracy ( -4 A). Digital Anemmeter AM400 with an accuracy f (0.1 m/) i ued t meaure the velcity f entering air t the tet ectin, the maximum velcity that the anemmeter can meaure i (0m/). A pht (1) hw the tet ectin, and fig. () illutrate the chematic drawing f the tet ectin.. Calculatin Prcedure The temperature f the in flw air t the tet ectin i within (0-) C. And the tet prcedure can be lited a fllw. 1- Turn n the air blwer in rder t upply the tet ectin with the required air. And the air flw i cntrlled eaily uing the cntrl valve that hwn in pht graph (1). - The tet ectin wa et t the prper temperature and thi wa achieved uing a variable tranfrmer. - After (- 4) minute the ytem wuld reach the teady tate cnditin. And thi technique wa adpted by (Al- Daher M. and A. H. Jaim, 00)(Al-Sammarai A. T. A., 1). Many reading fr the tube urface and al fr the inlet and utlet air and the libratry temperature have been regitered. The diameter f the filler (gla phere) wa meaured and fund t be (d=mm). And the prity f thi filler wa fund practically and fund t be (0.1), were phere rder in the tube i cnider t have randm arrangement and when thi wa cmpared with the value that calculated by uing the fllwing equatin(al- Daher M.. A, 000):- 0 ISSN E-ISSN 1-1
4 Mdern Applied Science Vl., N. ; April 0 dp * D...(1) And thi equal t (0.7), and the deference between the tw value (meaured and calculated) i fund t be negligible. Therefre the permeability wa calculated uing the fllwing equatin(b. Bunm, G. Fglia, O. Manca& S. Nardini, 00):- dp K... () 17(1 ) There are many variable have been calculate me f them i lcally indirectly meaured uch a Nuelt number and heat tranfer cefficient and the ther in between variable have been calculated e.g. clet number (), Rayeigh number (Ra) and Richardn number (Ri). Then the lcal heat tranfer cefficient wa calculated uing the fllwing equatin(huein A. Mhammed and Yain K. Salman, 007):- q hz.. () T T b z Where (q) i the heat flux fr a unit f area and thi i calculated frm the fllwing equatin:- Q q... (4) A. Where A.D.L. () And the bulk temperature fr the air wa calculated uing the fllwing equatin(j. P. Hlman, 177):- Ti T Tb ( ) () The characteritic f the flwing air were calculated thrugh the tet ectin which were variable depending n in the bulk temperature f the flwing air and thi were calculated uing the fllwing empirical equatin(jhn H. Lienhrd IV and Jhn H. Lienhrd V, 00):- f * Tb.1.. (7) * *Tb 4.47* Tb 4 f 1.77* 1.* Tb..() 1.* Tb.* Tb kf * Tb.().7* Tb.* Tb Prf. 1.1* Tb.() 4.7* Tb.* Tb Cpf. 1.7Tb () * Tb.0* Tb Where the quantity f the added heat tranfer (Q) frm the air wa calculated a fllw:- Q m Cpf (T T i). (1) And the generated heat (Pwr in ) in the heater wa fund a flw:- Pwr in I*V () The percentage f the heat tranfer heat l culd calculated a flw:- Q (1 ).(14) Pwrin And the lcal Nuelt number wa calculated uing the fllwing equatin:- Publihed by Canadian Center f Science and Educatin 1
5 Mdern Applied Science Vl., N. ; April 0 h D z Nu z.(1) ke Where k e i the effective cefficient f thermal cnductivity fr the pru media which culd be calculated a fllw(b. Bunm, G. Fglia, O. Manca& S. Nardini, 00)( C. Y. Chi and F. A. Kulacki, 1):- ke kf (1 ) k p.. (1) Where k f and k p i the thermal cnductivity f the air and pru media repectively. The thermal cnductivity f the air wa calculated uing equatin (). Reynld number (Re) wa calculated a fllw(al- Daher M.. A. 000):- f udp Re. (17) f 1 And clet number () wa calculated a fllw:- Re Pr f....(1) And Prandtl number (Pr f ) wa calculated depending n the change f the bulk temperature f the air uing equatin ().Grahf number (Gr) wa calculated a fllw(dnald A. Nield and Adrian Bejan, 1)(B. Bunm, G. Fglia, O. Manca& S. Nardini, 00)( C. Y. Chi and F. A. Kulacki, 1):- g KqD Gr (1) k 1 Where T b Rayleigh number (Ra) wa calculated uing the fllwing equatin:- Ra Gr Pr f...(0) Where Richardn number (Ri) wa calculated uing the fllwing equatin:- Ri Gr Re.. (1) And the average value f Nuelt number wa calculated a fllw:- dz....() L Five tete had been cared ut fr the fllwing rang (.1 1.4) f clet number. And fr each value f thi number the upplied heat wa changed. And thi wa fr three quantitie f the heat flux and al the flw wa (1.4,. and 1.)W/m. And thi wa depending n the upplied electricity vltage that ued fr heating the tet ectin the previu tet had been repeated ne fr each f the fllwing tube pitin (hrizntal and inclined with deferent angle)(0, 4, ). The relatinhip between the change f tube urface temperature and the tube length, fr each tet pitin were pltted. Al the relatin between average Nuelt number and clet number, fr a fixed value f a Rayleigh number were pltted. And a relatin between average Nuelt number and Rayleigh number fr fixed value f a clet number were pltted. 4. Reult and Dicuin Sixty tet had been carried ut fr each f the fllwing variable. 1) The angle ( ) f the tube have been change t have different value. Thee value were (0, 0, 4, ). ) clet number have been varied within the range (. 1.4) and thi wa dne five time. ) Rayleigh number have been varied within the range (.4-7.7) and thi wa dne three time. The relatinhip between f the tube urface temperature and it length fr the hrizntal pitin fr deferent value f heat flux were preented n fig. (). Thi figure hw that the tube urface temperature increae prprtinal with tube length. And thi with a linear manner. Except few pint at the tw end f the tube. And thi exceptin i increaed fr high value f Rayleigh number. And thi i believed i due t that bundary layer tart frm zer at ne end f the tube and it thickne i increaed t reach it peak me were between the tw end. The decreae in the tube urface temperature at the ut flw end i jutified by the heat l at that regin. The ame behavir wuld cntinue fr the fig. (4, and )which are fr the angle (0, 4 and ). And it can L e ISSN E-ISSN 1-1
6 Mdern Applied Science Vl., N. ; April 0 be nte that the tube urface temperature increae with the increae f the angle f the tube inclinatin and thi i due t the decreae f the thickne f the bundary layer, in additin t abrbed heat by the flwing air. The ht air ettle in the upper pace f the pru media and the cld air ettle in the bttm pace f the pru media. The height difference in the tube urface temperature i ( T=4. C). Thi wa regitered fr the firt heat flux and thi wa fr the pitin between ( =0) and ( = ). And the height difference fr the ecnd heat flux wa (( T=1.1 C). And the height difference fr the third heat flux wa ( T=.). Fig. (7,, and ) hw the relatinhip between the urface temperature and the tube length fr different value f clet number. The little difference between clet number value i related t the thermal prpertie which can be calculated fr each value f bulk temperature. And thu wa clarified in previuly (experimental wrk), in the equatin (7,,, and ). And fr thi relatinhip fr the hrizntal pitin and the ther angled pitin. It can be nticed that the tube urface temperature increaed with the increae f the tube length fr the different value f the heat flux. The maximum increae wa fr the maximum value f heat flux. And al the maximum difference fr the tube urface temperature wa regitered fr each tube pitin and they were fund t be: 0, T. C 0, T.1 C 4, T C, T 7.1 C Fig. () hw the ditributin f the tube urface temperature with it length fr all the tube inclinatin angle and fr (=1) and heat flux (q=.w/m ). It i clear frm thi figure that the tube urface temperature increae with the increae f the tube length. And thi increae ha a large tep fr a higher inclinatin angle f the tube. The highet temperature fr the tube urface regiter wa (T=7.4 C). The ame previu temperature ditributin and the ame tube pitin and fr (=0) and heat flux (q=1.w/m ) are preented in fig. (1). The highet temperature that regitered fr the tube urface wa (T=14. C) and thi, fr the tube pitin ( = ). The ditributin f the lcal Nuelt number with the tube length, fr different tube pitin and fr the firt heat flux (q=1.4w/m ) were preented n fig. (, 14, 1 and 1). It can be nticed that at me reading that the lcal Nuelt number i decreaed it thermal fully develped. And the regin thugh t be related t phenmenn f flw and thi i due t the exitence f the gla phere. Al culd be ntice be that the increae f clet number caue an increae in lcal Nuelt number, and thi i becaue f the bundary layer i thin. S the effect f the natural cnvectin increae at lw flw peed. And the height value f Nuelt number wa the hrizntal pitin f the tube and it decreae when the inclinatin angle f the tube increae t reach it maximum value (Nu=7.) at ( = ). The relatinhip between lcal Nuelt number with tube length fr all tube pitin are preented n fig. (17, 1, 1 and 0) at the heat flux (q=1.w/m ). It i clear that lcal Nuelt number behave in the ame manr a in the previu cae. And all it value are cled t each ther. And the rean i becaue cnvergence f the lcal cefficient f the heat tranfer, and thi i a reult frm cnvergence f the difference in the temperature value. The average value f Nuelt number had been calculated by ching the cnvergence value f temperature in the mid ectin f the tube where the air flw wa cnidered thermally fully develped. That becaue the imple difference between the temperature value near t the tube end. The increae f Rayleigh number caue cniderable increae in the average value f Nuelt number a hwn in fig.1, and. And thi wa fr all the tube pitin, except inclinatin with ( ) angle. And thi wa dwn fr different value f clet number which have been teted. Thi i becaue that the effect f natural cnvectin which ha a (parablic relatin) which i the cmmn hape fr all heat tranfer cnditin f thi rt. Publihed by Canadian Center f Science and Educatin
7 Mdern Applied Science Vl., N. ; April 0 The highet Nuelt number i crrepnding t the highet clet number. And thi i fr all tube inclinatin angle. And the average value f Nuelt number crrepnding t the mall Rayleigh number are cnvergence and the difference between the increaed at higher value f Rayleigh number. The relatinhip between Nuelt number and the average clet number fr different Rayleigh number fr all the tube pitin a hwn in fig.4,, and 7). Frm all thee curve, it i clear that the average Nuelt number increae with the increae f clet number and thi fr all cnditin. And the larget Nuelt number i crrepnding t the high value f Rayleigh number. Al frm thee figure it i pible t lcate, the heat tranfer regin (by natural cnvectin) and thi i dived int three regin, the firt i the left end f the curve. It can be een that the value f Nuelt number i ettle and thi cntinue t a certain pint right t the firt pint in the curve. S thi regin i the natural cnvectin zne which han t any effect fr clet number and there i n effect fr Reynld number. And Rayleigh number nly play the mater rle in thi mater. The ecnd regin t the right f the firt ne i the mixed cnvectin zne in thi regin it culd be een that the change f the Nuelt number give a change in the clet and Rayleigh number gather. And the third regin which i the right prtin f the curve, end it culd be een that a large change in Nuelt number value give light change in the value f Rayleigh number, i., e. thi regin i a frced cnvectin zne. Fig. (7,, and 0) give a clear picture t the effect f clet number fr different value f Rayleigh number. It culd be een that the average Nuelt number i increaed with the increae f Rayleigh number and thi i fr all the tube pitin. And the increae f the Nuelt number ha a large tep crrepnding t a large Rayleigh number pecially at the hrizntal tube pitin.. Cncluin Frm thi tudy the fllwing cncluin be deduced:- 1) The tudy urface temperature increae with increae f the heat flux and thi increae with larger tep at higher f the tube inclinatin angle. Thi i becaue the Phenmenn f eparating the cld air t be ettle in the bttm and the ht air t be ettle in the upreme. ) The tube urface temperature fr mall clet number i higher than that fr large value f clet number. And thi i true fr all value f heat flux. ) The value f lcally Nuelt number have it highet value fr the cae f hrizntal pitin f the tube. And thi i large value f Rayleigh number. 4) Lcal Nuelt number increae with the increae f clet number all the tube pitin. ) Thi fr teady we fund that there are three regin f cnvectin thi i depending f the change f Nuelt number and thi depend f clet number. And thi i fr the teted value f Rayleigh number which i hwn in table 1, fr all the teted tube pitin. ) An empirical relatin between the average value f Nuelt number with average clet number and average value f Rayleigh number. And thi fr all tube pitin. Thi empirical frmal:- Nu av Ra av a c1 c b av....() av All the cntant f the previu frmal are hwn in table. Recnditin 1) Studying the effect f the changing the cr ectin f the teted tube (elliptical, quare, triangle, etc..) ectin. ) Studying the effect f the changing the teting tube diameter. ) Studying the effect f the change the grain diameter. 4) Studying the effect f the uing grain with different diameter. ) Studying the effect f the change flwing fluid phae, e. g. uing vapr. Reference Al- Daher M. and A. H. Jaim. (00). A Theretical and Experimental Study n Laminer Frced Cnvectin Heat Tranfer Thrugh a Hrizntal Tube Filled with Pru Media, Scientific Jurnal f Tikrit, 00. c 4 ISSN E-ISSN 1-1
8 Mdern Applied Science Vl., N. ; April 0 Al- Daher M.. A. (000). Heat Tranfer by Mixed Cnvectin Thrugh the Hrizntal Circular Tube Filled with Pru Media, phd. Thei, Univerity f Technlgy, Baghdad, Iraq, 000. Al-Sammarai A. T. A. (1). Experimental tudy f frced cnvectin Heat Tranfer frm a Heated Cylinder in Free and Embedded Hrizntal Cylinder Array in a Pru Medium in Cr Flw, M.Sc. Thei, Univerity f Tikrit, Tikrit, Iraq, 1. B. Bunm, G. Fglia, O. Manca& S. Nardini. (00). Numerical Study n Mixed Cnvectin a Channel with an Open Cavity Filled with Pru Media, th Eurpean Thermal- Science Cnference, Vl., pp 1-, 00. B. C. Chandraekhara and P. M. S. Nambdiri. (00). Influence f Variable rmeability n Cmbine Free and Frced Cnvectin abut Inclined Surface in Pru Media, Internatinal Jurnal f Heat and Ma Tranfer, Vl., Iue, pp 1-0, January 1, Available nline 00. C. Y. Chi and F. A. Kulacki. (1). Mixed Cnvectin Thrugh Vertical Pru Annuli Lcally Heated frm the Inner Cylinder, Jurnal f Heat Ma Tranfer, Vl., pp 14-, 1. Dnald A. Nield and Adrian Bejan. (1). Cnvectin in Pru Media, Secnd Editin, Springer, pp 14-7, pp 1-4, 1. Huein A. Mhammed and Yain K. Salman. (007). Experimental Mixed Cnvectin fr Dwnward Laminar Flw in the Thermal Entrance Regin f Inclined and Vertical Circular Tube, Experimental Thermal and Fluid Science, pp 1-1, February 007, J. P. Hlman. (177). Experimental Methd fr Engineer, McGraw- Hill Bk cmpany th Editin, 177. Jhn H. Lienhrd IV and Jhn H. Lienhrd V. (00). A Heat Tranfer Text Bk, Third editin, Jhn H., pp 714, 00, Lienhrd. Nawaf H. Saeid. (004). Analyi f Mixed Cnvectin in a Vertical Pru Layer uing Nn-Equilibrium Mdel, Internatinal Jurnal f Heat and Ma Tranfer, Vl. 47, pp 1-7, July 004, Ping Cheng. (177). Cmbined Free and Cnvectin Flw abut Inclined urface in pru media, Internatinal Jurnal f Heat and Ma Tranfer, Vl. 0, Iue, pp 07-14, Augut 177, Available nline 00. W. L. Pu., P. Cheng and T. S. ha. (1). An Experimental Study f Mixed Cnvectin Heat Tranfer in Vertical Packed Channel, ALAA Jurnal f Thermphyic and Heat Tranfer, Vl. (4), pp. 17-1, 1 Y. M. F. El. Haadi, I. M. Rutum and A. Abdala. (00). Laminar Mixed Cnvectin in the Entrance Regin f Semicircular with Cntant Heat Flux, th ALAA/ASME/ Jurnal f Thermphyic and Heat Tranfer Cnference, 00. Table 1. Reult f Teting Tube Pitin Natural Frced Mixed cnvectin cnvectin cnvectin Hrizntal (0 ) <1. 1.<<.4 >.4 Inclined (0 ) < <<4.1 >4.1 Inclined (4 ) < <<. >. Inclined ( ).<<7. 7.<<.7 >.7 Publihed by Canadian Center f Science and Educatin
9 Mdern Applied Science Vl., N. ; April 0 Table. cntant f the previu frmal a b c1 c c = = = =0. Figure 1. A pht graph hwing the tet partie 1- Blwer, - Valve, - Tet Sectin, 4- Meter panel, - Vltage regular, - Vltmeter, 7- Ameter, - Thermmeter, - Flw meter Figure. Schematic drawing fr the tet rig including the tet ectin 1- Cncrete bae, - Blwer bae, - Blwer, 4- cnnecting tube, - Air valve, - Flange, 7- Fibber gla, ISSN E-ISSN 1-1
10 Mdern Applied Science Vl., N. ; April 0 T ( C) 4 4 q=1.4 W/m =.7 =1. =71. =. =. T ( C) 4 4 q=1.4 W/m =0. =17.00 =7.0 =4.1 = (A) q=. W/m q=. W/m (A) T ( C) 0 =.4 =1. =.7 =7.0 =4. T ( C) =.1 =14. =4.1 =0. = q=1. W/m =.1 =14. =.0 =04. =41.71 (B) q=1. W/m =0.1 =1. =41. =0. =4.4 (B) 0 T ( C) (C) Figure. The relatin between the tube urface temperature and it length fr many value f heat flux at many value f clet number at the hrizntal pitin f the tube (C) Figure 4. The relatin between the tube urface temperature and it length fr many value f heat flux at many value f clet number at the inclined angle (0 ) Publihed by Canadian Center f Science and Educatin 7
11 Mdern Applied Science Vl., N. ; April q=1.4 W/m =4. =1.4 =74.1 =41.4 = q=1.4 W/m =. =1. =7. =.7 = q=. W/m =. =1. =1.7 =. =4.1 (A) q=. W/m =. =1.00 =. =. =4. (A) q=1. W/m =. =14. =4.4 =00. =4.0 (B) (C) Figure. The relatin between the tube urface temperature and it length fr many value f heat flux at many value f clet number at the inclined angle (4 ) q=1. W/m =. =147. =41. =0. =4.4 (B) (C) Figure. The relatin between the tube urface temperature and it length fr many value f heat flux at many value f clet number at the inclined angle ( ) ISSN E-ISSN 1-1
12 Mdern Applied Science Vl., N. ; April =1. q=1. W/m q=. W/m q=1.4 W/m 10 =1. q=1. W/m q=1.4 W/m q=. W/m Figure 7. The relatin between the tube urface temperature and it length fr many value f heat flux fr =1. and hrizntal pitin f the tube =14.1 q=1. W/m q=. W/m q=1.4 W/m Figure. The relatin between the tube urface temperature and it length fr many value f heat flux fr =14.1 and inclinatin angle (0 ) =1.7 q=1. W/m q=. W/m q=1.4 W/m Figure. The relatin between the tube urface temperature and it length fr many value f heat flux fr =1.7 and inclinatin angle (4 ) Figure. The relatin between the tube urface temperature and it length fr many value f heat flux fr =1. and inclinatin angle ( ) 0 4 =1 q=. W/m Inclined Inclined 4 Inclined 0 Hrizntal Figure. The relatin between the tube urface temperature and it length fr all the tube pitin and fr the minimum value f heat flux q=1. W/m =0.00 Inclined Inclined 4 Inclined 0 Hrizntal Figure 1. The relatin between the tube urface temperature and it length fr all the tube pitin and fr the maximum value f heat flux Publihed by Canadian Center f Science and Educatin
13 Mdern Applied Science Vl., N. ; April 0 0 q=1.4 W/m 1 q=1.4 W/m =. =. =4.4 =0. 1 =71. =1. =.7 =41.1 =147. =. 7 0 Figure. The relatin between lcal Nuelt number and the tube length fr many value f clet number and hrizntal pitin f the tube at minimum heat flux q=1.4 W/m =4.4 =0. =41. =1. = Figure 1. The relatin between lcal Nuelt number and the tube length fr many value f clet number and inclinatin angle ( ) at minimum heat flux q=1. W/m =41.71 =04. =.04 =14. =. 1 Figure 14. The relatin between lcal Nuelt number and the tube length fr many value f clet number and inclinatin angle (0 ) at minimum heat flux q=1.4 W/m =. =41.4 =74.4 =1.4 =4. 1 Figure 1. The relatin between lcal Nuelt number and the tube length fr many value f clet number and inclinatin angle (4 ) at minimum heat flux Figure 17. The relatin between lcal Nuelt number and the tube length fr many value f clet number and hrizntal pitin f the tube at maximum heat flux q=1. W/m =4.4 =0. =41. =1. =0.1 Figure 1. The relatin between lcal Nuelt number and the tube length fr many value f clet number and inclinatin angle (0 ) at maximum heat flux 1 ISSN E-ISSN 1-1
14 Mdern Applied Science Vl., N. ; April q=1. W/m =4.0 =00. =4.4 =14. =. 1 =4.00 =. =.7 =14.1 =.47 1 Figure 1. The relatin between lcal Nuelt number and the tube length fr many value f clet number and inclinatin angle (4 ) at maximum heat flux q=1. W/m =4.4 =0. =41. =147. = Ra Figure. The relatin between average value f Nuelt number and Rayleigh number with changing the value f clet number fr the inclinatin angle (0 ) 1 =41. =. =.7 =1.7 =.0 1 Figure 0. The relatin between lcal Nuelt number and the tube length fr many value f clet number and inclinatin angle ( ) at maximum heat flux 1 1 =4. =. =. =1. = Ra Figure. The relatin between average value f Nuelt number and Rayleigh number with changing the value f clet number fr the inclinatin angle (4 ) 1 Hrizntal 14 1 Ra=01.7 Ra=4. Ra= Ra Figure 1. The relatin between average value f Nuelt number and Rayleigh number with changing the value f clet number fr the hrizntal pitin f tube Figure 4. The relatin between average value f Nuelt number and clet number fr the hrizntal pitin and fr different value f Rayleigh number Publihed by Canadian Center f Science and Educatin 141
15 Mdern Applied Science Vl., N. ; April Inclined 0 Ra=0.1 Ra=. Ra=1.4 1 Ra=. Hrizntal Inclined 0 Inclined 4 Inclined av Nu Figure. The relatin between average value f Nuelt number and clet number fr inclinatin angle (0 ), and fr different value f Rayleigh number Inclined 4 Ra=0.4 Ra=4. Ra= Figure. The relatin between average value f Nuelt number with clet number fr Rayleigh number (Ra=.) fr all tube pitin 1 Ra=4. Hrizntal Inclined 0 Inclined 4 Inclined Figure. The relatin between average value f Nuelt number and clet number fr inclinatin angle (4 ), and fr different value f Rayleigh number 1 Inclined Ra=.4 Ra=4.7 Ra= Figure. The relatin between average value f Nuelt number with clet number fr Rayleigh number (Ra=4.) fr all tube pitin Ra=.4 Hrizntal Inclined 0 Inclined 4 Inclined Figure 7. The relatin between average value f Nuelt number and clet number fr inclinatin angle ( ), and fr different value f Rayleigh number Figure 0. The relatin between average value f Nuelt number with clet number fr Rayleigh number (Ra=.4) fr all tube pitin 14 ISSN E-ISSN 1-1
Name Student ID. A student uses a voltmeter to measure the electric potential difference across the three boxes.
Name Student ID II. [25 pt] Thi quetin cnit f tw unrelated part. Part 1. In the circuit belw, bulb 1-5 are identical, and the batterie are identical and ideal. Bxe,, and cntain unknwn arrangement f linear
More informationChapter 9 Compressible Flow 667
Chapter 9 Cmpreible Flw 667 9.57 Air flw frm a tank thrugh a nzzle int the tandard atmphere, a in Fig. P9.57. A nrmal hck tand in the exit f the nzzle, a hwn. Etimate (a) the tank preure; and (b) the ma
More informationChapter 8 Sections 8.4 through 8.6 Internal Flow: Heat Transfer Correlations. In fully-developed region. Neglect axial conduction
Chapter 8 Sectin 8.4 thrugh 8.6 Internal Flw: Heat Tranfer Crrelatin T v cu p cp ( rt) k r T T k x r r r r r x In fully-develped regin Neglect axial cnductin u ( rt) r x r r r r r x T v T T T T T u r x
More informationChapter 8. Root Locus Techniques
Chapter 8 Rt Lcu Technique Intrductin Sytem perfrmance and tability dt determined dby cled-lp l ple Typical cled-lp feedback cntrl ytem G Open-lp TF KG H Zer -, - Ple 0, -, -4 K 4 Lcatin f ple eaily fund
More informationChapter 3. Electric Flux Density, Gauss s Law and Divergence
Chapter 3. Electric Flu Denity, Gau aw and Diergence Hayt; 9/7/009; 3-1 3.1 Electric Flu Denity Faraday Eperiment Cncentric phere filled with dielectric material. + i gien t the inner phere. - i induced
More informationShort notes for Heat transfer
Furier s Law f Heat Cnductin Shrt ntes fr Heat transfer Q = Heat transfer in given directin. A = Crss-sectinal area perpendicular t heat flw directin. dt = Temperature difference between tw ends f a blck
More informationTHE INFLUENCE OF SURFACE INCLINATION ON THE CALIBRATION OF SURFACE TEMPERATURE SENSORS
Prceeding, XVII IMEKO Wrld Cngre, June 22 27, 2003, Dubrvnik, Cratia Prceeding, XVII IMEKO Wrld Cngre, June 22 27, 2003, Dubrvnik, Cratia XVII IMEKO Wrld Cngre Metrlgy in the 3 rd Millennium June 22 27,
More information7-84. Chapter 7 External Forced Convection
Chapter 7 External Frced Cnvectin 7-99 Wind i blwing ver the rf f a hue. The rate f heat tranfer thrugh the rf and the ct f thi heat l fr -h perid are t be deterined. Auptin Steady perating cnditin exit.
More informationNONISOTHERMAL OPERATION OF IDEAL REACTORS Plug Flow Reactor. F j. T mo Assumptions:
NONISOTHERMAL OPERATION OF IDEAL REACTORS Plug Flw Reactr T T T T F j, Q F j T m,q m T m T m T m Aumptin: 1. Hmgeneu Sytem 2. Single Reactin 3. Steady State Tw type f prblem: 1. Given deired prductin rate,
More informationExaminer: Dr. Mohamed Elsharnoby Time: 180 min. Attempt all the following questions Solve the following five questions, and assume any missing data
Benha University Cllege f Engineering at Banha Department f Mechanical Eng. First Year Mechanical Subject : Fluid Mechanics M111 Date:4/5/016 Questins Fr Final Crrective Examinatin Examiner: Dr. Mhamed
More informationFlipping Physics Lecture Notes: AP Physics 1 Review of Kinematics
Flipping Phyic Lecture Nte: AP Phyic 1 Review f Kinematic AP i a regitered trademark f the Cllege Bard, which wa nt invlved in the prductin f, and de nt endre, thi prduct. Intrductry Cncept: Vectr: Magnitude
More informationAdvanced Heat and Mass Transfer by Amir Faghri, Yuwen Zhang, and John R. Howell
6.5 Natural Cnvectin in Enclsures Enclsures are finite spaces bunded by walls and filled with fluid. Natural cnvectin in enclsures, als knwn as internal cnvectin, takes place in rms and buildings, furnaces,
More informationProjectile Motion. What is projectile? Projectile -Any object which projected by some means and continues to move due to its own inertia (mass).
Prjectile Mtin AP Phyic B What i prjectile? Prjectile -Any bject which prjected by me mean and cntinue t me due t it wn inertia (ma). 1 Prjectile me in TWO dimenin Since a prjectile me in - dimenin, it
More informationFlipping Physics Lecture Notes: Simple Harmonic Motion Introduction via a Horizontal Mass-Spring System
Flipping Physics Lecture Ntes: Simple Harmnic Mtin Intrductin via a Hrizntal Mass-Spring System A Hrizntal Mass-Spring System is where a mass is attached t a spring, riented hrizntally, and then placed
More informationME 315 Exam 2 Wednesday, November 11, 2015 CIRCLE YOUR DIVISION
ME 315 Exa edneday, Nveber 11, 015 Thi i a cled-bk, cled-nte exainatin. There i a frula heet rvided. Yu are al allwed t bring yur wn ne-age letter ize, dubleided crib heet. Yu ut turn ff all cunicatin
More informationStudy Group Report: Plate-fin Heat Exchangers: AEA Technology
Study Grup Reprt: Plate-fin Heat Exchangers: AEA Technlgy The prblem under study cncerned the apparent discrepancy between a series f experiments using a plate fin heat exchanger and the classical thery
More informationAn Empirical Study of Frost Accumulation Effects on Louvered-Fin, Microchannel Heat Exchangers
Purdue Univerity Purdue e-pub Internatinal Refrigeratin and Air Cnditining Cnference Schl f Mechanical Engineering 4 An Empirical Study f Frt Accumulatin Effect n Luvered-Fin, Micrchannel Heat Exchanger
More informationCANKAYA UNIVERSITY FACULTY OF ENGINEERING MECHANICAL ENGINEERING DEPARTMENT ME 313 HEAT TRANSFER
CANKAYA UNIVERSITY FACUTY OF ENGINEERING MECHANICA ENGINEERING DEPARTMENT ME 313 HEAT TRANSFER CHAPTER-3 EXAMPES 1) Cnsider a slab f thicness as illustrated in figure belw. A fluid at temperature T 1 with
More informationStudy on the Heat Transfer Performance of the Annular Fin under Condensing Conditions Abdenour Bourabaa, Malika Fekih, Mohamed Saighi
Study n the Heat Tranfer Perfrmance f the Annular Fin under Cndening Cnditin Adenur Buraaa, Malika Fekih, Mhamed Saighi Atract A numerical invetigatin f the fin efficiency and temperature ditriutin f an
More informationFlipping Physics Lecture Notes: Simple Harmonic Motion Introduction via a Horizontal Mass-Spring System
Flipping Physics Lecture Ntes: Simple Harmnic Mtin Intrductin via a Hrizntal Mass-Spring System A Hrizntal Mass-Spring System is where a mass is attached t a spring, riented hrizntally, and then placed
More informationconvection coefficient. The different property values of water at 20 C are given by: u W/m K, h=8062 W/m K
Practice rblems fr Cnvective Heat Transfer 1. Water at 0 C flws ver a flat late 1m 1m at 10 C with a free stream velcity f 4 m/s. Determine the thickness f bndary layers, lcal and average vale f drag cefficient
More informationON THE EFFECTIVENESS OF POROSITY ON UNSTEADY COUETTE FLOW AND HEAT TRANSFER BETWEEN PARALLEL POROUS PLATES WITH EXPONENTIAL DECAYING PRESSURE GRADIENT
17 Kragujevac J. Sci. 8 (006) 17-4. ON THE EFFECTIVENESS OF POROSITY ON UNSTEADY COUETTE FLOW AND HEAT TRANSFER BETWEEN PARALLEL POROUS PLATES WITH EXPONENTIAL DECAYING PRESSURE GRADIENT Hazem Ali Attia
More informationNATURAL CONVECTION HEAT TRANSFER FROM A HEAT SINK WITH FINS OF DIFFERENT CONFIGURATION
Internatinal Jurnal f Innvatin and Applied Studies ISSN 2028-9324 Vl. 9 N. 3 Nv. 2014, pp. 1043-1047 2014 Innvative Space f Scientific Research Jurnals http://www.ijias.issr-jurnals.rg/ NATURAL CONVECTION
More informationPhys101 Final Code: 1 Term: 132 Wednesday, May 21, 2014 Page: 1
Phys101 Final Cde: 1 Term: 1 Wednesday, May 1, 014 Page: 1 Q1. A car accelerates at.0 m/s alng a straight rad. It passes tw marks that are 0 m apart at times t = 4.0 s and t = 5.0 s. Find the car s velcity
More informationInformation for Physics 1201 Midterm I Wednesday, February 20
My lecture slides are psted at http://www.physics.hi-state.edu/~humanic/ Infrmatin fr Physics 1201 Midterm I Wednesday, February 20 1) Frmat: 10 multiple chice questins (each wrth 5 pints) and tw shw-wrk
More informationA Comparison of Correlations for Heat Transfer from Inclined Pipes
A Comparion of Correlation for Heat Tranfer from Inclined Pipe Krihperad Manohar Department of Mechanical and Manufacturing Engineering The Univerity of the Wet Indie St. Augutine, Trinidad and Tobago
More informationBuoyancy Effect on the Fully Developed Air Flow in Concentric Inclined Annulus
Internatinal Jurnal f Mechanical & Mechatrnics Engineering IJMME-IJENS Vl:3 N:0 46 Buyancy Effect n the Fully Develped Air Flw in Cncentric Inclined Annulus Asmaa Ali Hussein Lecturer Fundatin Of Technical
More informationNumerical Simulation of the Thermal Resposne Test Within the Comsol Multiphysics Environment
Presented at the COMSOL Cnference 2008 Hannver University f Parma Department f Industrial Engineering Numerical Simulatin f the Thermal Respsne Test Within the Cmsl Multiphysics Envirnment Authr : C. Crradi,
More informationsin θ = = y = r sin θ & cos θ = = x = r cos θ
Flipping Phyic Lecture Nte: Intrductin t Circular Mtin and Arc Length Circular Mtin imply take what yu have learned befre and applie it t bject which are mving alng a circular path. Let begin with a drawing
More informationGAUSS' LAW E. A. surface
Prf. Dr. I. M. A. Nasser GAUSS' LAW 08.11.017 GAUSS' LAW Intrductin: The electric field f a given charge distributin can in principle be calculated using Culmb's law. The examples discussed in electric
More informationBEAM LOADING EFFECTS IN PROTON LINACS. R. L. G1uckstern Yale University
Octber 21, 1963 BEAM LOADING EFFECTS IN PROTON LINACS R. L. G1ucktern Yale Univerity Intrductin A bunched beam f charged particle paing thrugh a cavity interact with the field in the cavity. It cuple,
More informationHEAT TRANSFER AND PRESSURE DROP CHARACTERISTICS OF A HORIZONTAL ANNULAR PASSAGE IN THE TRANSITIONAL FLOW REGIME
HEAT TRANSFER AND PRESSURE DROP CHARACTERISTICS OF A HORIZONTAL ANNULAR PASSAGE IN THE TRANSITIONAL FLOW REGIME Ndenguma D.D., Dirker J.* and Meyer J.P. *Authr fr crrespndence Department f Mechanical and
More informationAssume that the water in the nozzle is accelerated at a rate such that the frictional effect can be neglected.
1 HW #3: Cnservatin f Linear Mmentum, Cnservatin f Energy, Cnservatin f Angular Mmentum and Turbmachines, Bernulli s Equatin, Dimensinal Analysis, and Pipe Flws Prblem 1. Cnservatins f Mass and Linear
More informationSediment transport mechanisms 1. Bed-load transport
10 Sediment tranprt mechanim 1. Bed-lad tranprt 10.1 Intrductin When the bed hear tre exceed a critical value, ediment are tranprted in the frm f bed-lad and upended lad. Fr bed-lad tranprt, the baic mde
More informationSPE Copyright 2005, Society of Petroleum Engineers
SPE 42 Numerical Simulatin f Fully Cupled Fluid-Flw/Gemechanical Defrmatin in Hydraulically Fractured Reervir J.G. Garcia, SPE, and L.W. Teufel, SPE, New Mexic Int. f Mining and Technlgy Cpyright 2, Sciety
More informationmaking triangle (ie same reference angle) ). This is a standard form that will allow us all to have the X= y=
Intrductin t Vectrs I 21 Intrductin t Vectrs I 22 I. Determine the hrizntal and vertical cmpnents f the resultant vectr by cunting n the grid. X= y= J. Draw a mangle with hrizntal and vertical cmpnents
More informationProcess Engineering Thermodynamics E (4 sp) Exam
Prcess Engineering Thermdynamics 42434 E (4 sp) Exam 9-3-29 ll supprt material is allwed except fr telecmmunicatin devices. 4 questins give max. 3 pints = 7½ + 7½ + 7½ + 7½ pints Belw 6 questins are given,
More informationGrumman F-14 Tomcat Control Design BY: Chike Uduku
Grumman F-4 Tmcat Cntrl Deign BY: Chike duku I. Atract SECTIONS II. III. IV. Deign jective eaured Cntant Deign V. Reult VI. VII. Cncluin Cmplete atla Cde I. Atract Deigning cntrller fr fighter jet i a
More informationChapter 9. Design via Root Locus
Chapter 9 Deign via Rt Lcu Intrductin Sytem perfrmance pecificatin requirement imped n the cntrl ytem Stability Tranient repne requirement: maximum verht, ettling time Steady-tate requirement :.. errr
More informationIntroductory Thoughts
Flw Similarity By using the Buckingham pi therem, we have reduced the number f independent variables frm five t tw If we wish t run a series f wind-tunnel tests fr a given bdy at a given angle f attack,
More informationBernoulli s equation may be developed as a special form of the momentum or energy equation.
BERNOULLI S EQUATION Bernoulli equation may be developed a a pecial form of the momentum or energy equation. Here, we will develop it a pecial cae of momentum equation. Conider a teady incompreible flow
More informationExtraction of Doping Profile in Substrate of MNOS capacitor Using Fast Voltage Ramp Deep Depletion C-V method
Iraqi Jurnal f Applied Phyic Abdulghefar K. Faiq Department f Phyic, Cllege f Science, Univerity f Salahaddin, Erbil, Kurditan Regin, Iraq Extractin f Dping Prfile in Subtrate f MNOS capacitr Uing Fat
More informationPlan o o. I(t) Divide problem into sub-problems Modify schematic and coordinate system (if needed) Write general equations
STAPLE Physics 201 Name Final Exam May 14, 2013 This is a clsed bk examinatin but during the exam yu may refer t a 5 x7 nte card with wrds f wisdm yu have written n it. There is extra scratch paper available.
More informationAdaptive finite element solution for the heat conduction with a moving heat source
Jurnal f Mechanical Science and Technlgy 6 () () 967~97 wwwpringerlinkcm/cntent/78-494x DOI 7/6--49- Adaptive finite element lutin fr the heat cnductin with a mving heat urce Chi-Kyung Kim * Department
More informationDisclaimer: This lab write-up is not
Diclaier: Thi lab write-up i nt t be cpied, in whle r in part, unle a prper reference i ade a t the urce. (It i trngly recended that yu ue thi dcuent nly t generate idea, r a a reference t explain cplex
More informationQ x = cos 1 30 = 53.1 South
Crdinatr: Dr. G. Khattak Thursday, August 0, 01 Page 1 Q1. A particle mves in ne dimensin such that its psitin x(t) as a functin f time t is given by x(t) =.0 + 7 t t, where t is in secnds and x(t) is
More informationNonisothermal Chemical Reactors
he 471 Fall 2014 LEUE 7a Nnithermal hemical eactr S far we have dealt with ithermal chemical reactr and were able, by ug nly a many pecie ma balance a there are dependent react t relate reactr ize, let
More information3D FE Modeling Simulation of Cold Rotary Forging with Double Symmetry Rolls X. H. Han 1, a, L. Hua 1, b, Y. M. Zhao 1, c
Materials Science Frum Online: 2009-08-31 ISSN: 1662-9752, Vls. 628-629, pp 623-628 di:10.4028/www.scientific.net/msf.628-629.623 2009 Trans Tech Publicatins, Switzerland 3D FE Mdeling Simulatin f Cld
More informationQ1. A string of length L is fixed at both ends. Which one of the following is NOT a possible wavelength for standing waves on this string?
Term: 111 Thursday, January 05, 2012 Page: 1 Q1. A string f length L is fixed at bth ends. Which ne f the fllwing is NOT a pssible wavelength fr standing waves n this string? Q2. λ n = 2L n = A) 4L B)
More informationMODULE 5 Lecture No: 5 Extraterrestrial Radiation
1 P age Principle and Perfrmance f Slar Energy Thermal Sytem: A Web Cure by V.V.Satyamurty MODULE 5 Lecture N: 5 Extraterretrial Radiatin In Mdule 5, Lecture N. 5 deal with 5.1 INTRODUCTION 5. EXTRA TERRESTRIAL
More informationElectric Current and Resistance
Electric Current and Resistance Electric Current Electric current is the rate f flw f charge thrugh sme regin f space The SI unit f current is the ampere (A) 1 A = 1 C / s The symbl fr electric current
More informationUnit code: H/ QCF level: 5 Credit value: 15 OUTCOME 3 - STATIC AND DYNAMIC FLUID SYSTEMS TUTORIAL 3 - VISCOSITY
Unit 43: Plant and Prcess Principles Unit cde: H/601 44 QCF level: 5 Credit value: 15 OUTCOME 3 - STATIC AND DYNAMIC FLUID SYSTEMS TUTORIAL 3 - VISCOSITY 3 Understand static and namic fluid systems with
More informationPHYS 314 HOMEWORK #3
PHYS 34 HOMEWORK #3 Due : 8 Feb. 07. A unifrm chain f mass M, lenth L and density λ (measured in k/m) hans s that its bttm link is just tuchin a scale. The chain is drpped frm rest nt the scale. What des
More informationFlipping Physics Lecture Notes: You Can t Run from Momentum
Flipping Phyic Lecture Nte: Yu Can t Run frm Mmentum Symbl fr mmentum i a lwercae p. p i fr the Latin wrd petere which mean t make fr, t travel t, t eek, r t purue. It pretty clear thi wrd i where the
More informationPhys102 Final-061 Zero Version Coordinator: Nasser Wednesday, January 24, 2007 Page: 1
Crdinatr: Nasser Wednesday, January 4, 007 Page: 1 Q1. Tw transmitters, S 1 and S shwn in the figure, emit identical sund waves f wavelength λ. The transmitters are separated by a distance λ /. Cnsider
More information1 Course Notes in Introductory Physics Jeffrey Seguritan
Intrductin & Kinematics I Intrductin Quickie Cncepts Units SI is standard system f units used t measure physical quantities. Base units that we use: meter (m) is standard unit f length kilgram (kg) is
More informationGain and Phase Margins Based Delay Dependent Stability Analysis of Two- Area LFC System with Communication Delays
Gain and Phae Margin Baed Delay Dependent Stability Analyi of Two- Area LFC Sytem with Communication Delay Şahin Sönmez and Saffet Ayaun Department of Electrical Engineering, Niğde Ömer Halidemir Univerity,
More informationCHAPTER 8b Static Equilibrium Units
CHAPTER 8b Static Equilibrium Units The Cnditins fr Equilibrium Slving Statics Prblems Stability and Balance Elasticity; Stress and Strain The Cnditins fr Equilibrium An bject with frces acting n it, but
More informationLesson Plan. Recode: They will do a graphic organizer to sequence the steps of scientific method.
Lessn Plan Reach: Ask the students if they ever ppped a bag f micrwave ppcrn and nticed hw many kernels were unppped at the bttm f the bag which made yu wnder if ther brands pp better than the ne yu are
More informationQ1. A) 48 m/s B) 17 m/s C) 22 m/s D) 66 m/s E) 53 m/s. Ans: = 84.0 Q2.
Phys10 Final-133 Zer Versin Crdinatr: A.A.Naqvi Wednesday, August 13, 014 Page: 1 Q1. A string, f length 0.75 m and fixed at bth ends, is vibrating in its fundamental mde. The maximum transverse speed
More informationCompressibility Effects
Definitin f Cmpressibility All real substances are cmpressible t sme greater r lesser extent; that is, when yu squeeze r press n them, their density will change The amunt by which a substance can be cmpressed
More informationExam 1 Solutions. Prof. Darin Acosta Prof. Selman Hershfield February 6, 2007
PHY049 Spring 008 Prf. Darin Acta Prf. Selman Herhfiel Februar 6, 007 Nte: Mt prblem have mre than ne verin with ifferent anwer. Be careful that u check ur eam againt ur verin f the prblem. 1. Tw charge,
More informationAircraft Performance - Drag
Aircraft Perfrmance - Drag Classificatin f Drag Ntes: Drag Frce and Drag Cefficient Drag is the enemy f flight and its cst. One f the primary functins f aerdynamicists and aircraft designers is t reduce
More informationLaPlace Transforms in Design and Analysis of Circuits Part 2: Basic Series Circuit Analysis
LaPlace Tranfrm in Deign and Analyi f Circuit Part : Baic Serie Circuit Analyi Cure N: E- Credit: PDH Thma G. Bertenhaw, Ed.D., P.E. Cntinuing Educatin and Develpment, Inc. 9 Greyridge Farm Curt Stny Pint,
More informationTransmission cost allocation in pool systems.
Tranmiin ct allcatin in pl ytem. Juli Uala Univeridad Carl III de Madrid Legané (Madrid), Spain juala@ing.uc3m.e Abtract The tranmiin ct allcatin prblem may be divided int three different ubprblem: the
More informationGeneral Chemistry II, Unit I: Study Guide (part I)
1 General Chemistry II, Unit I: Study Guide (part I) CDS Chapter 14: Physical Prperties f Gases Observatin 1: Pressure- Vlume Measurements n Gases The spring f air is measured as pressure, defined as the
More informationThermal analysis of Aluminum alloy Piston
Internatinal Jurnal f Emerging Trends in Engineering Research (IJETER), Vl. 3 N.6, Pages : 511-515 (2015) Special Issue f NCTET 2K15 - Held n June 13, 2015 in SV Cllege f Engineering, Tirupati http://warse.rg/ijeter/static/pdf/issue/nctet2015sp90.pdf
More informationbulk velocity through orifice,
150A Review Sessin Other Frictin Lsses Bernulli hf accunts fr all types f drag: is drag due t skin frictin is drag due t fittings (tabulated fractin f the velcity head) is drag due t units (a given r calculated
More informationNAME TEMPERATURE AND HUMIDITY. I. Introduction
NAME TEMPERATURE AND HUMIDITY I. Intrductin Temperature is the single mst imprtant factr in determining atmspheric cnditins because it greatly influences: 1. The amunt f water vapr in the air 2. The pssibility
More informationFabrication Thermal Test. Methodology for a Safe Cask Thermal Performance
ENSA (Grup SEPI) Fabricatin Thermal Test. Methdlgy fr a Safe Cask Thermal Perfrmance IAEA Internatinal Cnference n the Management f Spent Fuel frm Nuclear Pwer Reactrs An Integrated Apprach t the Back-End
More informationChapter 7: 17, 20, 24, 25, 32, 35, 37, 40, 47, 66 and 79.
hapter 7: 17, 0,, 5,, 5, 7, 0, 7, 66 and 79. 77 A power tranitor mounted on the wall diipate 0.18 W. he urface temperature of the tranitor i to be determined. Aumption 1 Steady operating condition exit.
More informationCONVECTION IN MICROCHANNELS
CAPER. Intrductin CONVECION IN MICROCANNELS.. Cntinuu and hernaic ythei. Previu chater are baed n tw fundaental autin: () Cntinuu: Navier-Stke equatin, and the energy equatin are alicable () hernaic equilibriu:
More information, which yields. where z1. and z2
The Gaussian r Nrmal PDF, Page 1 The Gaussian r Nrmal Prbability Density Functin Authr: Jhn M Cimbala, Penn State University Latest revisin: 11 September 13 The Gaussian r Nrmal Prbability Density Functin
More informationNGSS High School Physics Domain Model
NGSS High Schl Physics Dmain Mdel Mtin and Stability: Frces and Interactins HS-PS2-1: Students will be able t analyze data t supprt the claim that Newtn s secnd law f mtin describes the mathematical relatinship
More informationSPH3U1 Lesson 06 Kinematics
PROJECTILE MOTION LEARNING GOALS Students will: Describe the mtin f an bject thrwn at arbitrary angles thrugh the air. Describe the hrizntal and vertical mtins f a prjectile. Slve prjectile mtin prblems.
More informationChapter 2 GAUSS LAW Recommended Problems:
Chapter GAUSS LAW Recmmended Prblems: 1,4,5,6,7,9,11,13,15,18,19,1,7,9,31,35,37,39,41,43,45,47,49,51,55,57,61,6,69. LCTRIC FLUX lectric flux is a measure f the number f electric filed lines penetrating
More informationChapter 4. Unsteady State Conduction
Chapter 4 Unsteady State Cnductin Chapter 5 Steady State Cnductin Chee 318 1 4-1 Intrductin ransient Cnductin Many heat transfer prblems are time dependent Changes in perating cnditins in a system cause
More informationLab 11 LRC Circuits, Damped Forced Harmonic Motion
Physics 6 ab ab 11 ircuits, Damped Frced Harmnic Mtin What Yu Need T Knw: The Physics OK this is basically a recap f what yu ve dne s far with circuits and circuits. Nw we get t put everything tgether
More information2 LU 5 u LU a. yf) LLt z< CN 3 a> 12 a> E D E m C 5 */» c E O O^Z CN 8!H U J z I f l n Hi it-jl u-> CN J a : * 7 O U < _ i u. t U J _j f - 3 0H!4> s I 6.1 IP = E E
More informationRotating Paddle Switch SITRANS LPS200. Functional Safety Manual 05/2016 SITRANS
Rtating Paddle Switch Functinal Safety Manual 05/2016 SITRANS Table f cntent 1. SCOPE... 2 1.1. DEVICE IDENTIFICATION... 2 1.2. APPLICABLE DOCUMENTS... 3 1.3. RESTRICTIONS... 3 2. DEVICE DESCRIPTION...
More informationLecture 13 - Boost DC-DC Converters. Step-Up or Boost converters deliver DC power from a lower voltage DC level (V d ) to a higher load voltage V o.
ecture 13 - Bt C-C Cnverter Pwer Electrnic Step-Up r Bt cnverter eliver C pwer frm a lwer vltage C level ( ) t a higher la vltage. i i i + v i c T C (a) + R (a) v 0 0 i 0 R1 t n t ff + t T i n T t ff =
More informationEffect of Temperature on Some Rheological Properties of Polyvinyl Pyrrolidone (PVP)
Egypt. J. Slid, Vl. (32), N. (1), (2009) 81 Effect f Temperature n Sme Rhelgical Prpertie f Plyvinyl Pyrrlidne (PVP) Suzanne R. Abud 1, Abdul Kareem1 J. Al- Bermany 2 and Naar Megahed 3 1) Phyic Department,
More information37 Maxwell s Equations
37 Maxwell s quatins In this chapter, the plan is t summarize much f what we knw abut electricity and magnetism in a manner similar t the way in which James Clerk Maxwell summarized what was knwn abut
More informationSTIFFNESS AND DAMPING PROPERTIES OF EMBEDDED MACHINE FOUNDATIONS
Numer Vlume 1 June 006 Jurnal f Engineering Dr. Thamir. Al-Aawi Dr. Raad. Al-Aawi Zuhair. Al-Jaeri Prf. / Civil Eng. Dept. Lecturer/ Civil Eng. Dept. Structural Engineer Cllege f Eng./ Univ. f Baghdad
More informationFree Vibrations of Catenary Risers with Internal Fluid
Prceeding Series f the Brazilian Sciety f Applied and Cmputatinal Mathematics, Vl. 4, N. 1, 216. Trabalh apresentad n DINCON, Natal - RN, 215. Prceeding Series f the Brazilian Sciety f Cmputatinal and
More informationEXAM #1 PHYSICAL SCIENCE 103 FALLF, 2017
OBJECTIVES 1. Ft Pressure EXAM #1 PHYSICAL SCIENCE 103 FALLF, 2017 Determine the surface area f an bject. Given the weight and surface area, calculate the pressure. 2. Measuring Vlume & Mass Prvided a
More information20 Faraday s Law and Maxwell s Extension to Ampere s Law
Chapter 20 Faraday s Law and Maxwell s Extensin t Ampere s Law 20 Faraday s Law and Maxwell s Extensin t Ampere s Law Cnsider the case f a charged particle that is ming in the icinity f a ming bar magnet
More informationQ1. In figure 1, Q = 60 µc, q = 20 µc, a = 3.0 m, and b = 4.0 m. Calculate the total electric force on q due to the other 2 charges.
Phys10 Secnd Majr-08 Zer Versin Crdinatr: Dr. I. M. Nasser Saturday, May 3, 009 Page: 1 Q1. In figure 1, Q = 60 µc, q = 0 µc, a = 3.0 m, and b = 4.0 m. Calculate the ttal electric frce n q due t the ther
More informationThe Journal of Supercritical Fluids
J. f Supercritical Fluids 7 (212) 75 89 ntents lists available at SciVerse ScienceDirect The Jurnal f Supercritical Fluids ju rn al h m epage: www.elsevier.cm/lcate/supflu Flw and heat transfer characteristics
More informationFluid-structure coupling analysis and simulation of viscosity effect. on Coriolis mass flowmeter
APCOM & ISCM 11-14 th December, 2013, Singapore luid-tructure coupling analyi and imulation of vicoity effect on Corioli ma flowmeter *Luo Rongmo, and Wu Jian National Metrology Centre, A*STAR, 1 Science
More informationMODULE 1. e x + c. [You can t separate a demominator, but you can divide a single denominator into each numerator term] a + b a(a + b)+1 = a + b
. REVIEW OF SOME BASIC ALGEBRA MODULE () Slving Equatins Yu shuld be able t slve fr x: a + b = c a d + e x + c and get x = e(ba +) b(c a) d(ba +) c Cmmn mistakes and strategies:. a b + c a b + a c, but
More informationPhy 212: General Physics II 1 Chapter 18 Worksheet 3/20/2008
Phy 1: General Physics II 1 hapter 18 rksheet 3/0/008 Thermal Expansin: 1. A wedding ring cmpsed f pure gld (inner diameter = 1.5 x 10 - m) is placed n a persn s finger (diameter = 1.5 x 10 - m). Bth the
More informationRelationships Between Frequency, Capacitance, Inductance and Reactance.
P Physics Relatinships between f,, and. Relatinships Between Frequency, apacitance, nductance and Reactance. Purpse: T experimentally verify the relatinships between f, and. The data cllected will lead
More information5 th grade Common Core Standards
5 th grade Cmmn Cre Standards In Grade 5, instructinal time shuld fcus n three critical areas: (1) develping fluency with additin and subtractin f fractins, and develping understanding f the multiplicatin
More information1. Transformer A transformer is used to obtain the approximate output voltage of the power supply. The output of the transformer is still AC.
PHYSIS 536 Experiment 4: D Pwer Supply I. Intrductin The prcess f changing A t D is investigated in this experiment. An integrated circuit regulatr makes it easy t cnstruct a high-perfrmance vltage surce
More informationThermodynamics Partial Outline of Topics
Thermdynamics Partial Outline f Tpics I. The secnd law f thermdynamics addresses the issue f spntaneity and invlves a functin called entrpy (S): If a prcess is spntaneus, then Suniverse > 0 (2 nd Law!)
More informationTo begin we first need to consider HOW SUBSTANCES ARE TRANSPORTED IN FLUIDS
MEMBRANES Backgrund All animal tiue uch a mucle i cmped f a grup f cell and the lutin bathing them, the intertitial fluid. Within the cell i the intracellular fluid and the cell i bunded by a thin membrane
More informationEXAM #1 PHYSICAL SCIENCE 103 Spring, 2016
OBJECTIVES 1. Ft Pressure EXAM #1 PHYSICAL SCIENCE 103 Spring, 2016 Determine the surface area f an bject. Given the weight and surface area, calculate the pressure. 2. Measuring Vlume & Mass Prvided a
More informationThe Influence of the Load Condition upon the Radial Distribution of Electromagnetic Vibration and Noise in a Three-Phase Squirrel-Cage Induction Motor
The Influence of the Load Condition upon the Radial Ditribution of Electromagnetic Vibration and Noie in a Three-Phae Squirrel-Cage Induction Motor Yuta Sato 1, Iao Hirotuka 1, Kazuo Tuboi 1, Maanori Nakamura
More informationPerformance analysis of heat exchanger with different types of fins
1. www.ierjournal.org International Engineering Reearch Journal (IERJ) Special Iue 3 Page 3-370, 201, ISSN 2395-121 ISSN 2395-121 Performance analyi of heat exchanger with different type of fin #1 Mi.
More information