Computational flowfield analyses of hypersonic problems with reacting boundary layer

A mathematical model able to deal with high temperature gas effects in hypersonic flow fields is presented. In order to assess this model, four typical hypersonic applications are considered. The numerical results are presented and compared with experimental data. The effects of the catalyticity of the materials on the heat fluxes are also highlighted.

[1]  Chul Park,et al.  Assessment of two-temperature kinetic model for ionizing air , 1987 .

[2]  J. Anderson,et al.  Hypersonic and High-Temperature Gas Dynamics , 2019 .

[3]  L. A. Anderson,et al.  Effect of surface catalytic activity on stagnation heat-transfer rates. , 1973 .

[4]  C. Wilke.  A Viscosity Equation for Gas Mixtures , 1950 .

[5]  A. Balakrishnan,et al.  Real-gas flowfields about three-dimensional configurations , 1985 .

[6]  P. Roe.  Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes , 1997 .

[7]  J. J. Bertin.  The effect of protuberances, cavities, and angle of attack on the wind-tunnel pressure and heat-transfer distribution for the Apollo command module , 1966 .

[8]  J. Muylaert,et al.  A review of European code-validation studies in high-enthalpy flow , 1999, Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences.

[9]  J. Stoer,et al.  Introduction to Numerical Analysis , 2002 .

[10]  Kendall E. Atkinson.  An introduction to numerical analysis , 1978 .

[11]  Thomas J. Horvath,et al.  Aeroheating Testing and Predictions for Project Orion CEV at Turbulent Conditions , 2008 .

[12]  Graham V. Candler,et al.  Thermo-chemical nonequilibrium effects on the aerothermodynamics of aerobraking vehicles , 1993 .

[13]  P. Roe.  CHARACTERISTIC-BASED SCHEMES FOR THE EULER EQUATIONS , 1986 .

[14]  Giuseppe Pezzella,et al.  Catalytic Effects on Non-Equilibrium Aerothermodynamics of a Reentry Vehicle , 2007 .

[15]  Richard J. Schwartz,et al.  Testing of the Crew Exploration Vehicle in NASA Langley's Unitary Plan Wind Tunnel , 2007 .

[16]  Davide Cinquegrana,et al.  Aerothermodynamic Analysis of an Apollo-like Reentry Vehicle , 2006 .

[17]  C. F. Curtiss,et al.  Molecular Theory Of Gases And Liquids , 1954 .

[18]  Edward A. Mason,et al.  COLLISION INTEGRALS FOR THE TRANSPORT PROPERTIES OF DISSOCIATING AIR AT HIGH TEMPERATURES , 1962 .

[19]  M. Perić,et al.  Computation of fluid flow with a parallel multigrid solver , 1993 .

[20]  Chul Park,et al.  A review of reaction rates in high temperature air , 1989 .

[21]  Richard A. Thompson,et al.  A review of reaction rates and thermodynamic and transport properties for the 11-species air model for chemical and thermal nonequilibrium calculations to 30000 K , 1989 .