CFD evaluation of Mach 17 HYPULSE scramjet combustor data

Autor:	Charles R. McClinton, Robert D. Bittner, Glenn J. Bobskill, David W. Riggins
Rok vydání:	1991
Předmět:	business.industry Hypersonic flight Mechanics Computational fluid dynamics Fuel injection symbols.namesake Mach number Heat flux Combustor symbols Scramjet Aerospace engineering Combustion chamber business
Zdroj:	3rd International Aerospace Planes Conference.
DOI:	10.2514/6.1991-5093
Popis:	Three-dimensional finite rate chemistry solutions are performed on a single fuel injector configuration. The results are compared with limited experimental data obtained from the HYPULSE expansion tube facility at simulated flight Mach 17 flow conditions. All comparisons, except for wall heat flux, were in excellent agreement. Key findings from this study are useful in interpretation of the experimental measurements.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::d5779e962e9a0d96b5686f45c89ac766 https://doi.org/10.2514/6.1991-5093 Zobrazit plný text záznamu