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Accuracy of flux-split algorithms in high-speed viscous flowsGAITONDE, D; SHANG, J. S.AIAA journal. 1993, Vol 31, Num 7, pp 1215-1221, issn 0001-1452Article

Computation of crossing shock/turbulent boundary layer interaction at mach 8.3NARAYANSWAMI, N; HORSTMAN, C. C; KNIGHT, D. D et al.AIAA journal. 1993, Vol 31, Num 8, pp 1369-1376, issn 0001-1452Article

Experimental analysis of reflected shock behavior over a wedge with surface roughness: local behaviorSUZUKI, T; ADACHI, T; KOBAYASHI, S et al.JSME international journal. Series B, fluids and thermal engineering. 1993, Vol 36, Num 1, pp 130-134, issn 1340-8054Article

Experimental investigations of hypersonic shock-boundary layer interactionHENCKELS, A; KREINS, A. F; MAURER, F et al.Zeitschrift für Flugwissenschaften und Weltraumforschung. 1993, Vol 17, Num 2, pp 116-124, issn 0342-068XArticle

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Parametrical investigation of the interaction between turbulent wall shear layers and normal shock waves, including separationKALDELLIS, J. K.Journal of fluids engineering. 1993, Vol 115, Num 1, pp 48-55, issn 0098-2202Article

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Solution of the steady Euler equations in a generalized Lagrangian formulationYANG, J. Y; HSU, C. A; HUI, W. H et al.AIAA journal. 1993, Vol 31, Num 2, pp 266-272, issn 0001-1452Article

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Treatment of vortex sheets for the transonic full-potential equationDANG, T. Q.International journal for numerical methods in fluids. 1993, Vol 16, Num 9, pp 777-791, issn 0271-2091Article

Nonlinear relaxation Navier-Stokes solver for three-dimensional, high-speed internal flowsEDWARDS, J. R; MCRAE, D. S.AIAA journal. 1993, Vol 31, Num 7, pp 1222-1228, issn 0001-1452Conference Paper

Shock/boundary-layer interaction control with vortex generators and passive cavityMCCORMICK, D. C.AIAA journal. 1993, Vol 31, Num 1, pp 91-96, issn 0001-1452Conference Paper

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Approximate formula of weak oblique shock wave angleHUA-SHU DOU; HSUEH-TING TENG.AIAA journal. 1992, Vol 30, Num 3, pp 837-839, issn 0001-1452Article

A study of supersonic flow over the ogival bodies with attached shock waves at zero incidenceTOMESCU, N. S.Revue roumaine des sciences techniques. Série de mécanique appliquée. 1992, Vol 37, Num 1, pp 59-74, issn 0035-4074Article

Experimental investigation of normal-shock/turbulent-boundary-layer interactions with and without mass removalMORRIS, M. J; SAJBEN, M; KROUTIL, J. C et al.AIAA journal. 1992, Vol 30, Num 2, pp 359-366, issn 0001-1452Article

NND schemes and their applications to numerical simulation of two- and three-dimensional flowsHANZIN ZHANG; FENGGAN ZHUANG.Advances in applied mechanics. 1992, Vol 29, pp 193-256, issn 0065-2156Article

Numerical simulation of shock wave interactions with channel bends and gas nonuniformitiesFURSENKO, A. A; SHAROV, D. M; TIMOFEEV, E. V et al.Computers & fluids. 1992, Vol 21, Num 3, pp 377-396, issn 0045-7930Article

On the effect of external flow and shear-layer thickness on the expansion cells of under-expanded supersonic circular jetsMICHALKE, A.European journal of mechanics. B, Fluids. 1992, Vol 11, Num 3, pp 363-381, issn 0997-7546Article

Shock-induced mixing of a light-gas cylinderJACOBS, J. W.Journal of Fluid Mechanics. 1992, Vol 234, pp 629-649, issn 0022-1120, 22 p.Article

A solution of the wave equations using real gasesWINTERBONE, D. E; PEARSON, R. J.International journal of mechanical sciences. 1992, Vol 34, Num 12, pp 917-932, issn 0020-7403Article