第6章_田辺.PDF
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- きゅういち うづき
- 7 years ago
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1 ( ) ( ) ( )
2 Tube
3 . MGLAB
4 1.5 mm ( )
5 NS u u x u u u u = u + u ( ) ( u + u ) u u u u = u + u x x x + NS u ( ρ s ρ ) g a F R = αv 0 FR V
6 a a a k0 k /0
7 MGLAB - ( ) NS CPU khz NS
8 1 ga ARFAcoustic Radiation Force Model ( ) DNSDirect Numerical Simulation DNS FLUENT 900 Hz 2 mm 2000 K DNS s ( DNS) ( ARF) db
9 130 db 140 db 2.22 s DNS NS ARF 1 = x u x u λ π λ π ρ ρ 4 sin 2 max 2 u max SPL 0.54 ARF DNS CPU DNS 1/1000 ARF
10 IHI IHI () 1. Influence of Acoustic Field on Droplet Combustion in Microgravity, Tanabe, M., Aoki, K., Sato, K. and Fujimori, T., NASA/CP , Influence of Standing Sound Wave on Droplet Combustion, Tanabe, M., Morita, T., Aoki, K., Satoh, K., Fujimori, T. and Sato, J., Proceedings of the Combustion Institute, Vol. 28, p.1007, Combustion of Isolated droplet in Standing Sound Wave, Morita, T.,Tanabe, M., Aoki, K., 4th JSME-KSME Thermal Engineering Conference, Vol. 1, p Effects of Standing Sound Wave on Droplet Combustion, Morita, T., Aoki, K., Satoh, K., Fujimori, T. and Tanabe, M., Microgravity Science and Technology, XIV/2, p.29, 2003.
11 5. Evaluation of Combustion Enhancement by Standing Sound Wave Using Microgravity, Tanabe, M., Kono, M., Sato, K., Fujimori, T. and Aoki, K., Proceedings of The 23rd ISTS (Selected Papers), Vol. 2, p. 1662, ,,,,, B, , p. 126, Droplet Combusiton in Standing Sound Wave, Tanabe, M., Kuwahara, T., Satoh, K., Fujimori, T., Sato, J. and Kono, M., Proceedings of the Combustion Institute, Vol.30, No. 2, p. 1957, Analysis on thermo-acoustic streaming field by CFD simulation, Tachi, k., Kuwahara, T., Tanabe, M., Proceedings of The 24th ISTS (Selected Papers), p.787, ,,,,, Vol.22, No. 1, p. 42, 2005.
75 unit: mm Fig. Structure of model three-phase stacked transformer cores (a) Alternate-lap joint (b) Step-lap joint 3 4)
3 * 35 (3), 7 Analysis of Local Magnetic Properties and Acoustic Noise in Three-Phase Stacked Transformer Core Model Masayoshi Ishida Kenichi Sadahiro Seiji Okabe 3.7 T 5 Hz..4 3 Synopsis: Methods of local
PowerPoint プレゼンテーション
0 1 2 3 4 5 6 1964 1978 7 0.0015+0.013 8 1 π 2 2 2 1 2 2 ( r 1 + r3 ) + π ( r2 + r3 ) 2 = +1,2100 9 10 11 1.9m 3 0.64m 3 12 13 14 15 16 17 () 0.095% 0.019% 1.29% (0.348%) 0.024% 0.0048% 0.32% (0.0864%)
4
4 5 6 7 + 8 = ++ 9 + + + + ++ 10 + + 11 12 WS LC VA L WS = LC VA = LC L L VA = LC L VA L 13 i LC VA WS WS = LC = VA LC VA VA = VA α WS α = VA VA i WS = LC VA i t t+1 14 WS = α WS + WS α WS = WS WS WS =
FR 34 316 13 303 54
FR 34 316 13 303 54 23 ( 1 14 ) ( 3 10 ) 8/4 8/ 100% 8 22 7 12 1 9 8 45 25 28 17 19 14 3/1 6/27 5000 8/4 12/2930 1 66 45 43 35 49 25 22 20 23 21 17 13 20 6 1 8 52 1 50 4 11 49 3/4/5 75 6/7/8 46 9/10/11
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Vol..3 2010 2 10 2
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2009-9-2.indd
Q No.1441 Q No.1442 Vol.33 NO.9 (2009) 30 (614) Q No.1443 Vol.33 NO.9 (2009) 31 (615) Q No.1444 Vol.33 NO.9 (2009) 32 (616) Vol.33 NO.9 (2009) 33 (617) Vol.33 NO.9 (2009) 34 (618) Q No.1445 Vol.33 NO.9
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09030549_001.図書館31-1
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Vol.14 98 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 62 63 64 65 66 67 68
野岩鉄道の旅
29th 5:13 5:34 5:56 6:00 6:12 6:20 6:21 6:25 6:29 6:31 6:34 6:38 6:40 6:45 6:52 6:56 7:01 7:07 7:11 7:32 7:34 7:50 7:58 8:03 8:17 8:36 8:44 5:50 5:54 6:15 6:38 6:39 6:51 6:59 6:59 7:03 7:08 7:08 7:11 7:15
2010 : M0107189 3DCG 3 (3DCG) 3DCG 3DCG 3DCG S
2010 M0107189 2010 : M0107189 3DCG 3 (3DCG) 3DCG 3DCG 3DCG S 1 1 1.1............................ 1 1.2.............................. 4 2 5 2.1............................ 5 2.2.............................
Contents
Simulation Engineering Solution s NS Plant Designing Corporation Contents 2014 1 2 2014 2014 3 4 2014 - i u j 2014 5 N= 0.3N =200 mm N=1581.9N 6 2014 Z Y X 2014 7 by Marc) 8 2014 CFDEM LIGGGHTS DEM CFD
: u i = (2) x i Smagorinsky τ ij τ [3] ij u i u j u i u j = 2ν SGS S ij, (3) ν SGS = (C s ) 2 S (4) x i a u i ρ p P T u ν τ ij S c ν SGS S csgs
![: u i = (2) x i Smagorinsky τ ij τ [3] ij u i u j u i u j = 2ν SGS S ij, (3) ν SGS = (C s ) 2 S (4) x i a u i ρ p P T u ν τ ij S c ν SGS S csgs](/thumbs/91/106610562.jpg ": u i = (2) x i Smagorinsky τ ij τ [3] ij u i u j u i u j = 2ν SGS S ij, (3) ν SGS = (C s ) 2 S (4) x i a u i ρ p P T u ν τ ij S c ν SGS S csgs")
15 C11-4 Numerical analysis of flame propagation in a combustor of an aircraft gas turbine, 4-6-1 E-mail: tominaga@icebeer.iis.u-tokyo.ac.jp, 2-11-16 E-mail: ntani@iis.u-tokyo.ac.jp, 4-6-1 E-mail: itoh@icebeer.iis.u-tokyo.ac.jp,
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Simulation Study of Interaction between Alfvén Eigenmodes and Energetic Particles (TAE ) TAE TAE MHD ITER We studied the interaction between Alfvén eigenmodes and energetic particles in fusion plasmas
第６２巻 第１号 平成２４年４月／石こうを用いた木材ペレット
Bulletin of Japan Association for Fire Science and Engineering Vol. 62. No. 1 (2012) Development of Two-Dimensional Simple Simulation Model and Evaluation of Discharge Ability for Water Discharge of Firefighting
