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Results: 1-4 |
Results: 4
HIGH-PERFORMANCE SUPERSONIC MISSILE INLET DESIGN USING AUTOMATED OPTIMIZATION
Authors: ZHA GC SMITH D SCHWABACHER M RASHEED K GELSEY A KNIGHT D HAAS M
Citation: Gc. Zha et al., HIGH-PERFORMANCE SUPERSONIC MISSILE INLET DESIGN USING AUTOMATED OPTIMIZATION, Journal of aircraft, 34(6), 1997, pp. 697-705
NUMERICAL STUDY OF 3-DIMENSIONAL FLOWS USING UNFACTORED UPWIND-RELAXATION SWEEPING ALGORITHM
Authors: ZHA GC BILGEN E
Citation: Gc. Zha et E. Bilgen, NUMERICAL STUDY OF 3-DIMENSIONAL FLOWS USING UNFACTORED UPWIND-RELAXATION SWEEPING ALGORITHM, Journal of computational physics, 125(2), 1996, pp. 425-433
3-DIMENSIONAL SHOCK BOUNDARY-LAYER INTERACTION USING REYNOLDS STRESS EQUATION TURBULENCE MODEL/
Authors: ZHA GC KNIGHT D
Citation: Gc. Zha et D. Knight, 3-DIMENSIONAL SHOCK BOUNDARY-LAYER INTERACTION USING REYNOLDS STRESS EQUATION TURBULENCE MODEL/, AIAA journal, 34(7), 1996, pp. 1313-1320
NUMERICAL-SOLUTIONS OF EULER EQUATIONS BY USING A NEW FLUX VECTOR SPLITTING SCHEME
Authors: ZHA GC BILGEN E
Citation: Gc. Zha et E. Bilgen, NUMERICAL-SOLUTIONS OF EULER EQUATIONS BY USING A NEW FLUX VECTOR SPLITTING SCHEME, International journal for numerical methods in fluids, 17(2), 1993, pp. 115-144
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