Validation of global aeropropulsive characteristics of integrated configurations

Autor:	Ignatii I. Mazhul, Frederic Chalot, Philippe Rostand, Yurii P. Gounko, Anatoly M. Kharitonov, Latypov Albert F, Mikhail I. Yaroslavtsev, Pierre Perrier
Rok vydání:	1998
Předmět:	Engineering geography geography.geographical_feature_category business.industry Flow (psychology) Process (computing) Mechanical engineering Combustion Inlet Numerical reconstruction symbols.namesake Mach number symbols Scramjet business
Zdroj:	8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
DOI:	10.2514/6.1998-1624
Popis:	An integrated scramjet experiment is proposed as an "Integration Validation Object." A model was tested in different facilities at ITAM with and without combustion. The behavior of the three-dimensional inlet was experimentally studied in great detail. As a first step in the validation process, we present the numerical reconstruction of the flow past the inlet at a Mach number of 6.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::ffa151ceb324684ca788ca697f5acb9b https://doi.org/10.2514/6.1998-1624 Zobrazit plný text záznamu