Research Catalog

Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle

Title
Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.
Author
Wing, David J.
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

Details

Additional Authors
Langley Research Center.
Description
1 v.
Series Statement
NASA technical memorandum ; 4574
Subject
  • Coanda effect
  • Convergent-divergent nozzles
  • Flow deflection
  • Fluidics
  • Jet thrust
  • Nozzle flow
  • Static tests
  • Thrust vector control
  • Two dimensional flow
  • Wind tunnel tests
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 95-0478-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:4574
OCLC
marcive32852183
Author
Wing, David J.
Title
Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
Series
NASA technical memorandum ; 4574
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 3 microfiches.
Added Author
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:4574
Research Call Number
READEX Microfiche NAS 1.15:4574
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