Computational analyses of the LIMX TBCC inlet high-speed flowpath /

Bibliographic Details

Main Author:	Dippold, Vance
Corporate Authors:	NASA Glenn Research Center, JANNAF Propulsion Meeting
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:	NASA technical memorandum ; 2012-217219.
Subjects:	Turbine engines. Cycles. Inlet flow. Supersonic combustion ramjet engines. Combustion chambers. High speed. Mass flow rate. Reynolds averaging. Free flow.
Online Access:	https://purl.fdlp.gov/GPO/gpo25003