An edition of Shock-tunnel combustor testing for hypersonic vehicles (1994)

Shock-tunnel combustor testing for hypersonic vehicles

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Shock-tunnel combustor testing for hypersonic ...
Mark Loomis
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Last edited by VacuumBot
August 9, 2012 | History
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An edition of Shock-tunnel combustor testing for hypersonic vehicles (1994)

Shock-tunnel combustor testing for hypersonic vehicles

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Publish Date
Publisher
MCAT Institute, National Aeronautics and Space Administration, National Technical Information Service, distributor
Language
English

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Subjects

Wind tunnel tests, Two dimensional flow, Hypersonic flow, Supersonic combustion ramjet engines, Propulsion system performance, Propulsion system configurations, Engine tests, Air breathing engines, Hypersonic speed, Combustion chambers, Hypersonic aircraft, Hypersonic inlets, Inlet nozzles, Mach number
Edition Availability
Cover of: Shock-tunnel combustor testing for hypersonic vehicles
Shock-tunnel combustor testing for hypersonic vehicles
1994, MCAT Institute, National Aeronautics and Space Administration, National Technical Information Service, distributor
Microform in English
Cover of: Shock-tunnel combustor testing for hypersonic vehicles
Shock-tunnel combustor testing for hypersonic vehicles
1994, MCAT Institute, National Aeronautics and Space Administration, National Technical Information Service, distributor
Microform in English
Cover of: Shock-tunnel combustor testing for hypersonic vehicles
Shock-tunnel combustor testing for hypersonic vehicles
1994, MCAT Institute, National Aeronautics and Space Administration, National Technical Information Service, distributor
Microform in English

Add another edition?

Book Details

Edition Notes

Distributed to depository libraries in microfiche.

Shipping list no.: 95-0068-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.

Published in
San Jose, Calif, [Washington, DC, Springfield, Va
Series
MCAT Institute final report -- 94-07., [NASA contractor report] -- NASA CR-196836.
Other Titles
Shock tunnel combustor testing for hypersonic vehicles.

The Physical Object

Format
Microform
Pagination
1 v.

ID Numbers

Open Library
OL17001315M
OCLC/WorldCat
32198098

Source records

Oregon Libraries MARC record

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History

Download catalog record: RDF / JSON / OPDS | Wikipedia citation
August 9, 2012 Edited by VacuumBot Updated format '[microform] /' to 'Microform'; Removed author from Edition (author found in Work)
December 15, 2009 Edited by WorkBot link works
April 22, 2009 Edited by ImportBot add OCLC number
September 27, 2008 Created by ImportBot Imported from Oregon Libraries MARC record