Research Catalog

Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle

Title
Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle [microform] / Scott C. Asbury and Craig A. Hunter.
Author
Asbury, Scott C.
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]

Details

Additional Authors
  • Hunter, Craig A.
  • Langley Research Center.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA/TP ; 1999-209093
Uniform Title
NASA technical paper ; 209093.
Subject
  • Convergent-divergent nozzles
  • Boundary layer separation
  • Wind tunnel nozzles
  • Wind tunnel tests
  • Nozzle flow
  • Oblique shock waves
  • Flow visualization
Note
  • Shipping list no.: 99-0723-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.60:209093
OCLC
marcive41949879
Author
Asbury, Scott C.
Title
Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle [microform] / Scott C. Asbury and Craig A. Hunter.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
Series
NASA/TP ; 1999-209093
NASA technical paper ; 209093.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.
Added Author
Hunter, Craig A.
Langley Research Center.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-H-15 (MF)
Sudoc No.
NAS 1.60:209093
Research Call Number
READEX Microfiche NAS 1.60:209093
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