Applied Computational Fluid Dynamics Techniques - Wiley Episode 2 Part 10 doc
Applied Computational Fluid Dynamics Techniques - Wiley Episode 1 Part 7 doc
... = h 6 21 12 , (8 .12 a) D 1 = a N i N j ,x = a 2 11 11 , (8 .12 b) D 2 =− N i ,x N j ,x dx =− 1 h 1 1 11 . (8 .12 c) Assembly of all element contributions yields h 6 21 1 41 1 41 12 · u 1 u 2 u 3 u 4 ,t = −a 2 11 10 1 10 1 11 · u 1 u 2 u 3 u 4 . ... (nested 1- D): 2h 6 (u 2 i 1 + 4u 2...
Ngày tải lên: 06/08/2014, 01:21
Applied Computational Fluid Dynamics Techniques - Wiley Episode 1 Part 8 docx
... quantities: 18 2 APPLIED COMPUTATIONAL FLUID DYNAMICS TECHNIQUES 0 0 .1 0.2 0.3 0.4 0.5 0.6 0.7 0 .8 0.9 1 1 .1 0 2 4 6 8 10 DENSITY X-COORDINATE Exact FEFLO -0 .2 0 0.2 0.4 0.6 0 .8 1 1.2 0 2 4 6 8 10 VELOCITY X-COORDINATE Exact FEFLO 0 0 .1 0.2 0.3 0.4 0.5 0.6 0.7 0 .8 0.9 1 1 .1 0 ... al. (19 84 )) u =tu ,t + t 2 2 u ,tt n+ . (8. 22) 16 8...
Ngày tải lên: 06/08/2014, 01:21
Applied Computational Fluid Dynamics Techniques - Wiley Episode 1 Part 9 doc
... (Weatherill et al. ( 19 93 b)); or - by evaluation of gradients (Whitaker et al. ( 19 89) , Luo et al. ( 19 93 , 19 94 a)). 204 APPLIED COMPUTATIONAL FLUID DYNAMICS TECHNIQUES A Galerkin or central-difference discretization ... combinations Velocity Pressure Operator p1 q0 ( 0, 1, 2, 1, 0) p1 p1 ( 1, 0, 2, 0, 1) iso-p1 p1 ( 1, 1, 4, 1, 1) In particular, we note that the p1...
Ngày tải lên: 06/08/2014, 01:21
Applied Computational Fluid Dynamics Techniques - Wiley Episode 1 Part 10 pptx
... SOLVERS 215 -0 .4 -0 .2 0 0.2 0.4 0.6 0.8 10 0 10 5 11 0 11 5 12 0 12 5 13 0 13 5 14 0 14 5 15 0 Vertical Force Time Explicit Advection Theta=0.50 Theta=0.60 Theta =1. 00 (c) -0 .4 -0 .3 -0 .2 -0 .1 0 0 .1 0.2 0.3 0.4 0 ... 3.08 Ex30.6 0. 012 16 60 3296 3.92 Ex50.8 0. 016 12 45 32 01 4.03 Ex 51. 2 0.025 830 15 46 8.36 Ex 51. 6 0.033 623 11 14 11 .60 Ex 5...
Ngày tải lên: 06/08/2014, 01:21
Applied Computational Fluid Dynamics Techniques - Wiley Episode 2 Part 1 docx
... notation of Figure 13 .19 , we can write x p = x 0 + i i g i , (13 .20 ) where g 1 ,2 = x 1 ,2 x 0 , g 3 = g 1 ì g 2 |g 1 ì g 2 | , (13 . 21 a,b) 1 ,2 = N 1 ,2 , 0 = 1 −α 1 − α 2 . (13 . 21 c,d) Point x p may ... (or L2 projection) N i 2 N j 2 d ˆu j2 = N i 2 N j 1 d ˆu j1 . (13 . 12 ) This may be expressed in matrix form as M c u 2 = r = Lu 1...
Ngày tải lên: 06/08/2014, 02:20
Applied Computational Fluid Dynamics Techniques - Wiley Episode 2 Part 2 pdf
... ADAPTIVE MESH REFINEMENT 27 9 1 12 Level 0 1 N 2 N 1 12 1 N 2 N 1 12 Level 1 1 N 2 N 1 12 1 N 2 N 33 3 N 3 N 1 12 1 N 2 N 1 12 1 N 2 N 3 3 N (c)(b)(a) (a) (b) (c) Figure 14 .2. Mesh enrichment (a) ... INTERPOLATION 26 7 Table 13 .2. Particle-mesh interpolation timings ON=F,OFF=V ON=F Particle-tracing time (s) 25 7.0 17.6 MFLOP-rate recorded 1.11 20 . 82 Total runn...
Ngày tải lên: 06/08/2014, 02:20
Applied Computational Fluid Dynamics Techniques - Wiley Episode 2 Part 3 pps
... 2. 92 2 .36 IBM-6000/ 530 1000 2- ChainTetra 2. 63 2. 62 IBM-6000/ 530 10 000 Edge 13. 4 1.00 IBM-6000/ 530 10 000 Triangle 7 .21 1.85 IBM-6000/ 530 10 000 Tetrahedron 5 .26 2. 54 IBM-6000/ 530 10 000 2- ChainTetra ... ipoi0-related arrays. However, such a specialized EFFICIENT USE OF COMPUTER HARDWARE 30 7 121 32 4 524 635 871089101111 1 nedge 121 32 4 524 635 871089101111 1 np...
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Applied Computational Fluid Dynamics Techniques - Wiley Episode 2 Part 4 pps
... Configuration: nedge =4, 179,771 mvecl % reduced i/a nvecl % reduced i/a nvecl 64 97 .22 63 97 .22 63 128 93.80 127 98.36 121 25 6 89 .43 25 5 97.87 22 3 5 12 86.15 510 97 . 24 3 84 1 0 24 82. 87 1018 96.77 608 20 48 79.30 20 26 ... 24 8 79 24 8 7– 12 23 776 23 776 13–18 7136 7136 19 24 0 21 44 25 –30 1 0 24 1 0 24 31–36 0 1 0 24 37– 42 0 336 Table 15.17. Inlet problem on...
Ngày tải lên: 06/08/2014, 02:20
Applied Computational Fluid Dynamics Techniques - Wiley Episode 2 Part 6 pot
... 360 APPLIED COMPUTATIONAL FLUID DYNAMICS TECHNIQUES Mach-nr. (1. 025 , 3. 025 , 0.05) (a) (c) Mach-nr. (1. 025 , 3. 025 , 0.05) ( b ) Figure 16. 6. Macro-blocking: (a) one layer ... 1.00 Seque 518 1.17 10 30 22 7 2. 69 20 30 21 8 2. 80 Block 1 26 0 2. 35 420 00 elements respectively. The residual curves for the three different cases are compared in Figure 16. 8(e). As one c...
Ngày tải lên: 06/08/2014, 02:20
Applied Computational Fluid Dynamics Techniques - Wiley Episode 2 Part 6 pps
... Aftosmis et al. (20 00), LeVeque and Calhoon (20 01), Dadone and Grossman (20 02) , Baum et al. (20 03), - Euler with boundary layer corrections: Aftosmis et al. (20 06) , - low-Reynolds-number laminar ... layers; Applied Computational Fluid Dynamics Techniques: An Introduction Based on Finite Element Methods, Second Edition. Rainald Lửhner â 20 08 John Wiley & Sons,...
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Applied Computational Fluid Dynamics Techniques - Wiley Episode 2 Part 7 pot
... APPLIED COMPUTATIONAL FLUID DYNAMICS TECHNIQUES pressure 7. 000e-01 4. 375 e-01 1 .75 0e-01 -8 .75 0e-01 -3 .500e-01 pressure 7. 000e-01 4. 375 e-01 1 .75 0e-01 -8 .75 0e-01 -3 .500e-01 abs(vel) 1.100e+00 8 .25 0e-01 5.500e-01 2. 75 0e-01 0.000e+00 abs(vel) 1.100e+00 8 .25 0e-01 5.500e-01 2. 75 0e-01 0.000e+00 (e) -0 .2 ... 4 07 pressure 7. 000e-01 4. 375 e-0...
Ngày tải lên: 06/08/2014, 02:20
Applied Computational Fluid Dynamics Techniques - Wiley Episode 2 Part 8 docx
... APPLIED COMPUTATIONAL FLUID DYNAMICS TECHNIQUES -4 0 -2 0 0 20 40 60 80 100 120 0 20 40 60 80 100 120 140 160 180 20 0 22 0 Position Time x_c -5 0 5 10 15 20 25 30 35 -4 0 -2 0 0 20 40 60 80 100 120 z-Position x-Position x_c ... wave elevation at the hull 426 APPLIED COMPUTATIONAL FLUID DYNAMICS TECHNIQUES (e) (f) -0 .1 -0 . 08 -0...
Ngày tải lên: 06/08/2014, 02:20
Applied Computational Fluid Dynamics Techniques - Wiley Episode 2 Part 9 docx
... Kroo ( 199 3),Crispin ( 199 4),Quagliarella and Cioppa ( 199 4), Quagliarella ( 199 5), Doorly ( 199 5), Periaux ( 199 5), Yamamoto and Inoue ( 199 5), Vicini and Quagliarella ( 199 7, 199 9), Obayashi ( 199 8), Obayashi ... ( 198 5), Jameson ( 198 8, 199 5), Kuruvila et al. ( 199 5), Reuther and Jameson ( 199 5), Reuther et al. ( 199 6), Anderson and Venkata- krishnan ( 199 7), Elliott and P...
Ngày tải lên: 06/08/2014, 02:20
Applied Computational Fluid Dynamics Techniques - Wiley Episode 2 Part 10 doc
... Roundtable (1998). 478 APPLIED COMPUTATIONAL FLUID DYNAMICS TECHNIQUES -0 .07 -0 .06 -0 .05 -0 .04 -0 .03 -0 . 02 -0 .01 0 -0 .08 -0 .06 -0 .04 -0 . 02 0 0. 02 0.04 0.06 0.08 (a) (b) Figure 20 .13. Wigley hull: ... France, May 23 28 (20 04). Huyse, L. and R.M. Lewis. Aerodynamic Shape Optimization of Two-Dimensional Airfoils Under Uncertain Co...
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Applied Computational Fluid Dynamics Techniques - Wiley Episode 2 Part 11 potx
... Problems; AIAA-0 2- 0451 (20 02) . Soto, O., R. Löhner and J.R. Cebral. An Implicit Monolithic Time Accurate Finite Element Scheme for Incompressible Flow Problems; AIAA-0 1 -2 626 -CP (20 01). Soto, ... for CFD; AIAA-0 2- 0 8 62 (20 02) . Tilch, R., A. Tabbal, M. Zhu, F. Dekker and R. Löhner. Combination of Body-Fitted and Embedded Grids for External Vehicle Aerodynamics; AIAA-0 7-1...
Ngày tải lên: 06/08/2014, 02:20