Research Catalog

Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft

Title
Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft [microform] / W.G. Steenken ... [et al.].
Publication
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]

Details

Additional Authors
  • Steenken, W. G.
  • Hugh L. Dryden Flight Research Center.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA/TM ; 1999-206572
Uniform Title
NASA technical memorandum ; 206572.
Alternative Title
Factors affecting inlet engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
Subject
  • F-18 aircraft
  • Aerodynamic stability
  • Angle of attack
  • Compressors
  • Control surfaces
  • Flight control
  • Research vehicles
  • Rotors
  • Subsonic speed
Note
  • Shipping list no.: 99-0685-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:206572
OCLC
marcive41964667
Title
Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft [microform] / W.G. Steenken ... [et al.].
Imprint
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
Series
NASA/TM ; 1999-206572
NASA technical memorandum ; 206572.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 3 microfiches.
Added Author
Steenken, W. G.
Hugh L. Dryden Flight Research Center.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:206572
Research Call Number
READEX Microfiche NAS 1.15:206572
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