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Experimental Aerodynamic Characteristics at Mach Numbers From 0.60 to 2.70 of Two Supersonic Cruise Fighter Configurations

Samuel M. Dollyhigh
Format
Book; Government Document
Published
Washington, D.C. : 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 Technical Memorandum
SuDoc Number
NAS 1.15:78764
Description
187 p. : ill. ; 27 cm.
Notes
  • "Langley Research Center, Hampton, Virginia."
  • Feb. 1979.
Series Statement
NASA technical memorandum 78764
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Aerodynamics, Supersonic.
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    a| Supersonic wind tunnels.
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    a| Fighter planes x| Design and construction.
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