Analytic corrections to CFD heating predictions accounting for changes in surface catalysis
暂无分享,去创建一个
[1] G. Inger,et al. Nonequilibrium Stagnation Point Boundary Layers with Arbitrary Surface Catalycity , 1963 .
[2] P. A. Gnoffo,et al. Point-implicit relaxation strategies for viscous, hypersonic flows , 1989 .
[3] Aeroassisted Flight Experiment aerodynamic characteristics at flight conditions , 1990 .
[4] George R. Inger,et al. Nonequilibrium Boundary-Layer Effects on the Aerodynamic Heating of Hypersonic Waverider Vehicles , 1995 .
[5] Peter A. Gnoffo,et al. Navier-Stokes simulations of Orbiter aerodynamic characteristics including pitch trim and bodyflap , 1994 .
[6] Paul Kolodziej,et al. Thermal response of integral multicomponent composite thermal protection systems , 1985 .
[7] J. Elder,et al. Recombination-Dominated Nonequilibrium Heat Transfer to Arbitrarily Catalytic Hypersonic Vehicles , 1991 .
[8] Peter Gnoffo,et al. A code calibration program in support of the Aeroassist Flight Experiment , 1989 .
[9] C. Angelopoulos. High resolution schemes for hyperbolic conservation laws , 1992 .
[10] R. Goulard,et al. On Catalytic Recombination Rates in Hypersonic Stagnation Heat Transfer , 1958 .
[11] Peter A. Gnoffo,et al. Hypersonic entry heating with discontinuous surface catalycity - A combined analytic/CFD approach , 1996 .
[12] Paul Kolodziej,et al. Thermal response of integral multicomponent composite thermal protection systems , 1986 .
[13] P. Roe. Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes , 1997 .
[14] Peter A. Gnoffo,et al. Multiblock analysis for Shuttle Orbiter reentry heating from Mach 24 to Mach 12 , 1994 .
[15] P. Gnoffo. An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows , 1990 .
[16] H. C. Yee,et al. On symmetric and upwind TVD schemes , 1985 .
[17] Peter A. Gnoffo,et al. Application of the LAURA code for slender-vehicle aerothermodynamics , 1992 .