Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition /

Bibliographic Details

Main Author:	Slater, John W.
Corporate Authors:	NASA Glenn Research Center, AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference
Other Authors:	Saunders, John D.
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Series:	NASA technical memorandum ; 216362.
Subjects:	Computational fluid dynamics 241. Data simulation. Hypersonics. Static pressure. Supersonic combustion ramjet engines. Wind tunnel tests. Aerodynamics. Boundary layers.
Online Access:	https://purl.fdlp.gov/GPO/gpo4610