Item Details

Parametric Experimental Investigation of a Scramjet Nozzle at Mach 6 With Freon and Argon or Air Used for Exhaust Simulation

James M. Cubbage, William J. Monta
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Language
English
Series
NASA Technical Paper
Description
103 p. : ill. ; 28 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Bibliography: p. 11.
Series Statement
NASA technical paper ; 3048
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| Parametric experimental investigation of a scramjet nozzle at Mach 6 with freon and argon or air used for exhaust simulation / c| James M. Cubbage, William J. Monta.
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    a| Bibliography: p. 11.
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    a| Aerodynamics, Hypersonic.
    650
      
    0
    a| Aircraft exhaust emissions.
    650
      
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    a| Airplanes x| Ramjet engines x| Testing v| Statistics.
    650
      
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    a| Jet nozzles x| Testing v| Statistics.
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    a| Monta, William J.
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