An edition of Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system
(2001)
Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system
by J. R. DeBonis
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Publish Date
2001
Publisher
National Aeronautics and Space Administration, Glenn Research Center,
Available from NASA Center for Aerospace Information
Language
English
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Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system
2001, National Aeronautics and Space Administration, Glenn Research Center, Available from NASA Center for Aerospace Information
Microform
in English
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Book Details
Edition Notes
Shipping list no.: 2002-0157-M.
Also available via Internet from the NASA web site. Address as of 10/10/02: http://gltrs.grc.nasa.gov/reports/2001/TM-2001-210567.pdf ; current access is available via PURL.
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2001?] 1 microfiche.
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| January 21, 2010 | Edited by WorkBot | add subjects and covers |
| December 11, 2009 | Created by WorkBot | add works page |