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Results: 1-16 |
Results: 16
Vitamin A insufficiency accelerates the decrease in the number of sperm induced by an environmental disruptor, bisphenol A, in neonatal mice
Authors: Nakahashi, K Matsuda, M Mori, T
Citation: K. Nakahashi et al., Vitamin A insufficiency accelerates the decrease in the number of sperm induced by an environmental disruptor, bisphenol A, in neonatal mice, ZOOL SCI, 18(6), 2001, pp. 819-821
Flow simulation of NAL experimental supersonic airplane/booster separationusing overset unstructured grids
Authors: Togashi, F Nakahashi, K Ito, Y Iwamiya, T Shimbo, Y
Citation: F. Togashi et al., Flow simulation of NAL experimental supersonic airplane/booster separationusing overset unstructured grids, COMPUT FLU, 30(6), 2001, pp. 673-688
Flap-deflection optimization for transonic cruise performance improvement of supersonic transport wing
Authors: Kim, HJ Obayashi, S Nakahashi, K
Citation: Hj. Kim et al., Flap-deflection optimization for transonic cruise performance improvement of supersonic transport wing, J AIRCRAFT, 38(4), 2001, pp. 709-717
Simulation of vortex breakdown using adaptive grid refinement with vortex-center identification
Authors: Murayama, M Nakahashi, K Sawada, K
Citation: M. Murayama et al., Simulation of vortex breakdown using adaptive grid refinement with vortex-center identification, AIAA J, 39(7), 2001, pp. 1305-1312
Aerodynamic optimization of supersonic transport wing using unstructured adjoint method
Authors: Kim, HJ Sasaki, D Obayashi, S Nakahashi, K
Citation: Hj. Kim et al., Aerodynamic optimization of supersonic transport wing using unstructured adjoint method, AIAA J, 39(6), 2001, pp. 1011-1020
Real-coded adaptive range genetic algorithm and its application to aerodynamic design
Authors: Oyama, A Obayashi, S Nakahashi, K
Citation: A. Oyama et al., Real-coded adaptive range genetic algorithm and its application to aerodynamic design, JSME A, 43(2), 2000, pp. 124-129
Numerical analysis of scramjet internal flow by hybrid unstructured grid method
Authors: Kodera, M Igarashi, Y Nakahashi, K Kanda, T Hiraiwa, T Mitani, T
Citation: M. Kodera et al., Numerical analysis of scramjet internal flow by hybrid unstructured grid method, JSME I J B, 43(3), 2000, pp. 407-413
Inverse design of a thick supercritical airfoil
Authors: Pambagjo, TE Nakahashi, K Obayashi, S
Citation: Te. Pambagjo et al., Inverse design of a thick supercritical airfoil, T JPN SOC A, 43(140), 2000, pp. 61-66
Intergrid-boundary definition method for overset unstructured grid approach
Authors: Nakahashi, K Togashi, F Sharov, D
Citation: K. Nakahashi et al., Intergrid-boundary definition method for overset unstructured grid approach, AIAA J, 38(11), 2000, pp. 2077-2084
Inverse optimization of supersonic wing design with twist specification
Authors: Jeong, S Obayashi, S Nakahashi, K
Citation: S. Jeong et al., Inverse optimization of supersonic wing design with twist specification, INVERSE P E, 7(6), 1999, pp. 519-535
Drags in scramjet engine testing: Experimental and computational fluid dynamics studies
Authors: Mitani, T Kanda, T Hiraiwa, T Igarashi, Y Nakahashi, K
Citation: T. Mitani et al., Drags in scramjet engine testing: Experimental and computational fluid dynamics studies, J PROPUL P, 15(4), 1999, pp. 578-583
Applications of unstructured hybrid grid method to high-Reynolds number viscous flows
Authors: Nakahashi, K Sharov, D Kano, S Kodera, M
Citation: K. Nakahashi et al., Applications of unstructured hybrid grid method to high-Reynolds number viscous flows, INT J NUM F, 31(1), 1999, pp. 97-111
Inverse design of supersonic airfoils using integral equations
Authors: Jeong, S Matsushima, K Iwamiya, T Obayashi, S Nakahashi, K
Citation: S. Jeong et al., Inverse design of supersonic airfoils using integral equations, J AIRCRAFT, 36(3), 1999, pp. 606-608
Flow computations around delta wings using unstructured hybrid grids
Authors: Kano, S Nakahashi, K
Citation: S. Kano et K. Nakahashi, Flow computations around delta wings using unstructured hybrid grids, J AIRCRAFT, 36(2), 1999, pp. 374-379
Inverse design optimization of transonic wings based on multi-objective genetic algorithms
Authors: Takahashi, S Obayashi, S Nakahashi, K
Citation: S. Takahashi et al., Inverse design optimization of transonic wings based on multi-objective genetic algorithms, AIAA J, 37(12), 1999, pp. 1656-1662
Euler/Navier-Stokes optimization of supersonic wing design eased on evolutionary algorithm
Authors: Oyama, A Obayashi, S Nakahashi, K Nakamura, T
Citation: A. Oyama et al., Euler/Navier-Stokes optimization of supersonic wing design eased on evolutionary algorithm, AIAA J, 37(10), 1999, pp. 1327-1328
Risultati: 1-16 |