Development and characterization testing of an air pulsation valve for a pulse detonation engine supersonic parametric inlet test section /

Bibliographic Details

Main Author:	Tornabene, Robert
Corporate Author:	NASA Glenn Research Center
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2005]
Series:	NASA technical memorandum ; 213893.
Subjects:	Air flow. Characterization. Engine inlets. Pulse detonation engines. Supersonic wind tunnels. Gas valves. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo13800