Two-dimensional viscous flow computations of hypersonic scramjet nozzle flowfields at design and off-design conditions

Autor:	H. T. Lai, G. J. Harloff, E. S. Nelson
Rok vydání:	1988
Předmět:	Hypersonic speed Materials science business.industry Nozzle Heat transfer coefficient symbols.namesake Mach number Parasitic drag Heat transfer symbols Two-dimensional flow Scramjet Aerospace engineering business
Zdroj:	24th Joint Propulsion Conference.
Popis:	The PARC2D code has been selected to analyze the flowfields of a representative hypersonic scramjet nozzle over a range of flight conditions from Mach 3 to 20. The flowfields, wall pressures, wall skin friction values, heat transfer values and overall nozzle performance are presented.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::b767b036c8eb321db9336e71b8763134 https://doi.org/10.2514/6.1988-3280 Zobrazit plný text záznamu