AAAAAA
Results:
1-10
|
Results: 10
Authors:
Kim, KH
Kim, C
Rho, OH
Citation: Kh. Kim et al., Methods for the accurate computations of hypersonic flows - I. AUSMPW+ scheme, J COMPUT PH, 174(1), 2001, pp. 38-80
Authors:
Kim, KH
Kim, C
Rho, OH
Citation: Kh. Kim et al., Methods for the accurate computations of hypersonic flows - II. Shock-aligned grid technique, J COMPUT PH, 174(1), 2001, pp. 81-119
Authors:
Chae, D
Kim, C
Rho, OH
Citation: D. Chae et al., Reply to comment on "Development of an improved gas-kinetic BGK scheme forinviscid and viscous flows", J COMPUT PH, 171(2), 2001, pp. 848-850
Authors:
Ahn, T
Kim, HJ
Kim, C
Rho, OH
Citation: T. Ahn et al., Inverse design of transonic wings using wing planform and target pressure optimization, J AIRCRAFT, 38(4), 2001, pp. 644-652
Authors:
Ahn, J
Kim, HJ
Lee, DH
Rho, OH
Citation: J. Ahn et al., Response surface method for airfoil design in transonic flow, J AIRCRAFT, 38(2), 2001, pp. 231-238
Authors:
Kim, CS
Kim, C
Rho, OH
Citation: Cs. Kim et al., Sensitivity analysis for the Navier-Stokes equations with two-equation turbulence models, AIAA J, 39(5), 2001, pp. 838-845
Authors:
Kim, KH
Rho, OH
Park, C
Citation: Kh. Kim et al., Navier-Stokes computation of flows in arc heaters, J THERMOPHY, 14(2), 2000, pp. 250-258
Authors:
Chae, D
Kim, C
Rho, OH
Citation: D. Chae et al., Development of an improved gas-kinetic BGK scheme for inviscid and viscousflows, J COMPUT PH, 158(1), 2000, pp. 1-27
Authors:
Kim, CS
Kim, C
Rho, OH
Citation: Cs. Kim et al., Parallel computations of high-lift airfoil flows using two-equation turbulence models, AIAA J, 38(8), 2000, pp. 1360-1368
Authors:
Kim, HJ
Kim, C
Rho, OH
Citation: Hj. Kim et al., Multipoint inverse design method for transonic wings, J AIRCRAFT, 36(6), 1999, pp. 941-947
Risultati:
1-10
|