Rotating Detonation Engine Performance Model for Rocket Applications

Autor:	Alexis J. Harroun, Stephen D. Heister, David P. Stechmann
Rok vydání:	2019
Předmět:	business.product_category Materials science business.industry Detonation Aerospace Engineering Combustion Chamber pressure Propellant mass fraction Rocket Space and Planetary Science Mass flow rate Combustor Aerospace engineering Current (fluid) business
Zdroj:	Journal of Spacecraft and Rockets. 56:887-898
ISSN:	1533-6794 0022-4650
DOI:	10.2514/1.a34313
Popis:	A simplified theoretical treatment of rotating detonation engine (RDE) performance is developed for rocket applications with traceability to current combustion technology. In particular, the influe...
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::d07269074d0e0bd0d9b4fd42db79bc42 https://doi.org/10.2514/1.a34313 Zobrazit plný text záznamu