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Title
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Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system /
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Format
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online resource
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Internet Access
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https://purl.fdlp.gov/GPO/LPS23166
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Author
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DeBonis, James R., author.
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Published
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Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2001.
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SuDoc Number
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NAS 1.15:210567
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Item Number
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0830-D (online)
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Variation of Title
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Supersonic wind tunnel tests of a half-axisymmetric 12 degree spike inlet to a rocket-based combined-cycle propulsion system
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Description
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1 online resource (18 pages) : illustrations.
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Content Type
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text
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Series
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(NASA technical memorandum ; 2001-210567.)
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General Note
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"February 2001."
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"Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting sponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000."
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"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
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Bibliography
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Includes bibliographical references (page 5).
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Metadata Source
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Description based on online resource; title from PDF title page (NASA, viewed Nov. 13, 2017).
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Added Entry
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Trefny, Charles J., author.
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Added Entry
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NASA Glenn Research Center, issuing body.
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Linking Field
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Print version: Supersonic Wind Tunnel Tests of a Half-Axisymmetric 12 Deg-Spike Inlet to a Rocket-Based Combined-Cyc (OCoLC)640923504
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Microfiche version: DeBonis, James R. Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system (OCoLC)50765193
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URL
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Address at time of PURL creation https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20010056686.pdf
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Holdings
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All items
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OCLC Number
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(OCoLC)1011356298
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CGP Record Link
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https://catalog.gpo.gov:443/F/?func=direct&doc_number=001035311&local_base=GPO01PUB
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System Number
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001035311
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