Hypersonic flows for reentry problems
Jean-Antoine Désidéri, R. Glowinski, Jacques Périaux
Springer-Verlag, 1993 - Mathematics - 248 pages
The physical modelling and the numerical simulation of the critical reentry phase of hypersonic space vehicles are important areas of aerospace research. Eight specific problems of aerodynamics and thermodynamics were chosen as the central topics of this workshop. In these two volumes bothexperimental and computational data are collected along with comparative reviews presented at the meeting by international experts in the field of hypersonic flows. The books will be an important reference and the data will be valuable for numerical simulations of hypersonic flows and theirapplications in physics and engineering.
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Hypersonic Stability and Transition
Scattering Kernels for GasSurface Interaction
16 other sections not shown
AIAA AIAA Paper angle approximate similitude arc jet flow atoms axis blunt body Boltzmann Boltzmann equation boundary conditions boundary layer calculations coefficient collision computation Computational Fluid Dynamics constant contours density determine diagnostic diatomic dimensionless dissociation distribution energy enthalpy equations equilibrium Euler experimental data experiments Figure flight flow field Fluid free stream function grid heat flux hypersonic flows inlet interaction inviscid flows kernel laminar laser Mach number measurements method molecular molecule NASA Navier-Stokes Navier-Stokes equations nitrogen nonequilibrium nozzle obtained parameters particles perfect gas physical plane pressure probe problem propulsion radiation ramp react real gas real gas effects recombination reentry represented Reynolds number rotational scale scattering Scramjet shock layer shock tube shock wave simulation species stagnation stagnation point stagnation pressure supersonic surface Sutherland's law techniques thermal Thomson scattering three-dimensional transition turbulence upstream validation variables vehicle velocity vibrational viscous wall wind tunnel