Development and characterization testing of an air pulsation valve for a pulse detonation engine supersonic parametric inlet test section [electronic resource] / Robert Tornabene.

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Bibliographic Details
Online Access:	Online Access Online Access
Main Author:	Tornabene, Robert
Corporate Author:	NASA Glenn Research Center
Format:	Government Document Electronic 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.

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Call Number:	NAS 1.15:2005-213893
NAS 1.15:2005-213893	Available