Item Details

Static Thrust-Vectoring Performance of Nonaxisymmetric Convergent-Divergent Nozzles With Post-Exit Yaw Vanes

Robert J. Foley, Odis C. Pendergraft, Jr.
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
iii, 77 p. : ill. ; 28 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Bibliography: p. 11.
Series Statement
NASA technical paper ; 3085
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes / c| Robert J. Foley, Odis C. Pendergraft, Jr.
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    a| NASA technical paper ; v| 3085
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    a| Bibliography: p. 11.
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    a| Airplanes x| Motors x| Thrust.
    650
      
    0
    a| Yawing (Aerodynamics)
    650
      
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    a| Blades.
    650
      
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    a| Jet nozzles x| Testing.
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    a| Pendergraft, Odis C.
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