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Validation of Scramjet Exhaust Simulation Technique at Mach 6

H. B. Hopkins, W. Konopkaz, and J. Leng
Format
Book; Government Document
Published
Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1979.
Language
English
Series
NASA Contractor Report
SuDoc Number
NAS 1.26:3003
Description
xiv, 90 p. : ill. ; 27 cm.
Notes
  • "Prepared for Langley Research Center under contract NAS1-14152."
  • Includes bibliographical references.
Series Statement
NASA contractor report 3003
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Validation of scramjet exhaust simulation technique at Mach 6 / c| H. B. Hopkins, W. Konopkaz, and J. Leng.
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    a| xiv, 90 p. : b| ill. ; c| 27 cm.
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    0
    a| Hypersonic planes.
    650
      
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    a| Airframes.
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    a| Aircraft exhaust emissions.
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    1
      
    a| Konopka, W.
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    a| Leng, J.
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    a| United States. b| National Aeronautics and Space Administration. b| Scientific and Technical Information Office.
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