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

Subjects:

  • 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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Hoffett Field, California , USA One Worthrop Avenue Top inlet flow field and engine-inlet performance data for an advanced fighter aircraft coafigu- ration were obtained over the Mach to range. These studies ~t oaly provided extensive data for the baseline arrangerent. Purchase Bird Strike - 1st Edition. Print Book & E-Book. ISBN , Cross-flow fans are a unique type of turbomachinery, since both suction and discharge occur radially. The research in this field, which includes several theoretical and experimental studies, has not led yet to an ultimate set of criteria about the design, which is still based on empirical methods deriving from previous by: develop the aerospace field and the CFD field too. Keywords— ANSYS Flu ANSYS ICEM Drag Coefficient (C D), F Aircraft, Lift Coefficient (C L), Mach number and Velocity. I. INTRODUCTION A. F Aircraft The F Fighting Falcon is a combat, multi-role fighter aircraft. It is highly manoeuvrable and has proven itself inFile Size: KB.