Thermophysical Aspects of Re-entry FlowsJames N. Moss, Carl D. Scott American Institute of Aeronautics and Astronautics, Incorporated, 1986 - Technology & Engineering - 626 pages |
Contents
LowDensity Aerothermodynamics | 3 |
Direct Simulation Monte Carlo Method and Comparison | 25 |
Drag of Bodies in Rarefied Hypersonic Flow | 44 |
Copyright | |
21 other sections not shown
Common terms and phrases
Aeroassisted Orbital Transfer AIAA AIAA Paper angle of attack AOTV ARCFLO atom body boundary layer bow shock calculated Chemical Physics collision computed cone continuum convective cross sections curve density dissociation downstream drag drag coefficient DSMC e-N₂ effect ELECTRON ENERGY enthalpy equations equilibrium experimental flat plate flight flowfield flux free molecular freestream gage heat transfer heat-transfer rate heating distribution heating rates Hypersonic Flow increase interaction inviscid Knudsen number laminar leading edge leeward heating Mach number measured molecules Morse potential N₂ NASA nonequilibrium nosetip obtained Orbital Transfer Vehicles parameter particle predicted present pressure radiation radiative rate coefficients rate constants ratio reaction reattachment regime Reynolds number rotational scattering shock layer shock wave shown in Fig simulation solution species stagnation point stagnation region strong interaction surface temperature theory thermal three-dimensional tion transition Turb turbulent upstream values velocity viscous wall wind tunnel windward centerline