Research Catalog

Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability

Title
Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability [microform] / Mary L. Mason and James R. Burley II.
Author
Mason, Mary L.
Publication
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.

Details

Additional Authors
  • Burley, James R.
  • United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Description
1 v.
Series Statement
NASA technical paper ; 2559
Subject
  • Airplanes > Motors > Thrust
  • Jet nozzles > Testing
  • Pitching (Aerodynamics)
  • Short take-off and landing aircraft
  • Axisymmetric flow
  • Nozzle geometry
  • Nozzle thrust coefficients
  • Short takeoff aircraft
  • Static tests
  • Thrust vector control
Bibliography (note)
  • Includes bibliographical references.
Reproduction (note)
  • Microfiche.
Call Number
GPO Microfiche NAS 1.60:2559
OCLC
marcive56619770
Author
Mason, Mary L.
Title
Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability [microform] / Mary L. Mason and James R. Burley II.
Imprint
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
Series
NASA technical paper ; 2559
Bibliography
Includes bibliographical references.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1986. 1 microfiche.
Added Author
Burley, James R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Gpo Item No.
0830-H-15 (MF)
Sudoc No.
NAS 1.60:2559
Research Call Number
GPO Microfiche NAS 1.60:2559
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