Research Catalog

Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes

Title
Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes [microform] / Robert J. Foley, Odis C. Pendergraft, Jr.
Author
Foley, Robert J.
Publication
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]

Details

Additional Authors
  • Pendergraft, Odis C.
  • Langley Research Center.
Description
iii, 77 p. : ill.; 28 cm.
Series Statement
NASA technical paper ; 3085
Subject
  • Convergent-divergent nozzles
  • Jet vanes
  • Nozzle geometry
  • Static tests
  • Static thrust
  • Thrust vector control
  • Yaw
  • Jet nozzles > Testing
  • Blades
  • Yawing (Aerodynamics)
  • Airplanes > Motors > Thrust
Note
  • Prepared at Langley Research Center.
Bibliography (note)
  • Bibliography: p. 11.
Reproduction (note)
  • Microfiche.
Call Number
GPO Microfiche NAS 1.60:3085
OCLC
marcive34350214
Author
Foley, Robert J.
Title
Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes [microform] / Robert J. Foley, Odis C. Pendergraft, Jr.
Imprint
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]
Series
NASA technical paper ; 3085
Bibliography
Bibliography: p. 11.
Reproduction
Microfiche. Washington, D.C. : National Aeronautics and Space Administration, 1991. 2 microfiche.
Added Author
Pendergraft, Odis C.
Langley Research Center.
Gpo Item No.
0830-H-15 (MF)
Sudoc No.
NAS 1.60:3085
Research Call Number
GPO Microfiche NAS 1.60:3085
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