NASA NTRS · 19890046260
Modeling of hypersonic reacting flows
Abstract
The importance of thermochemical nonequilibrium in hypersonic flow is studied as well as the breakdown of a one-temperature kinetic model. Consideration is given to vibration relaxation, reaction rates, and conservation equations for chemical variables. Experimental data on the pitching moment characteristics of the raked-off blunted elliptic cone geometry proposed for use with an aeroassisted orbit transfer vehicle are presented.
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Park, Chul. 1989-01-01. Modeling of hypersonic reacting flows. https://ntrs.nasa.gov/citations/19890046260
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