Shock tunnel studies of scramjet phenomena 1994. Supplements 11 and 12 [microform]

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Bibliographic Details
Corporate Author:	United States. National Aeronautics and Space Administration
Format:	Government Document Microfilm Book
Language:	English
Published:	[Brisbane, Australia] : [Washington, D.C.] : [Springfield, Va.] : University of Queensland ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], [1995]
Series:	NASA contractor report ; NASA CR-199445.
Subjects:	Boundary layers. Enthalpy. Gas expansion. Hypersonic flow. Nozzle flow. Shock tubes. Shock tunnels. Skin friction. Stress waves. Supersonic combustion. Supersonic combustion ramjet engines. Thrust measurement.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:199445
NAS 1.26:199445	Restricted Place a Hold