Theoretical and experimental engine-inlet flow fields for fighter forebodies
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Theoretical and experimental engine-inlet flow fields for fighter forebodies by Steven F. Yaros

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Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English


  • Fighter planes.,
  • Aerodynamics, Supersonic.,
  • Aerodynamics, Transonic.

Book details:

Edition Notes

StatementSteven F. Yaros.
SeriesNASA technical paper -- 2270.
ContributionsUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
The Physical Object
Pagination63 p. :
Number of Pages63
ID Numbers
Open LibraryOL17830297M

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The capability of two numerical methods, one for transonic and one for supersonic flows, to predict the flow fields about representative fighter aircraft forebodies in the vicinity of the engine inlets was examined. The Mach number range covered was to and the Author: S. F. Yaros. Theoretical and experimental engine-inlet flow fields for fighter forebodies / By Steven F. Yaros and United States. National Aeronautics and Space Administration. February \. - NASA TP i I c.1 i I Steven F. 'Yaros '. Theoretical and Experimental Engine-Inlet Flow Fields for Fighter Forebodies Steven F. Yaros Langley Research Center Hampton, Virginia. a INTRODUCTION. Modeling and Identification of Large Sideslip Effects from Flight Experiments Theoretical and experimental engine-inlet flow fields for fighter forebodies to predict the flow fields about.

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