Nonequilibrium Viscous Shock-Layer Heat Transfer with Arbitrary Surface Catalycity

Autor: R. L. Baker, George R. Inger
Rok vydání: 2005
Předmět:
Zdroj: Journal of Spacecraft and Rockets. 42:193-200
ISSN: 1533-6794
0022-4650
DOI: 10.2514/1.7568
Popis: An approximate yet accurate analysis of aerodynamic heating at a highly cooled stagnation region, which embraces the entire high-altitude hypersonic flight regime where nonequilibrium dissociation/recombination in the shock layer and finite surface catalysis effects are both important, is given. Closed-form relationships are given for the relative nonequilibrium effects that are convenient for cost-effective engineering studies of high-altitude hypervelocity vehicle heating.
Databáze: OpenAIRE