Research Catalog

Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

Title
Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control [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.
Description
1 v.
Series Statement
NASA/TM ; 1999-209513
Uniform Title
NASA technical memorandum ; 209513.
Alternative Title
Static performance of a fixed geometry exhaust nozzle incorporating porous cavities for shock boundary layer interaction control
Subject
  • Exhaust nozzles
  • Porosity
  • Hole geometry (Mechanics)
  • Cavities
  • Thrust vector control
Note
  • Shipping list no.: 2000-0197-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:209513
OCLC
marcive43263577
Author
Asbury, Scott C.
Title
Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control [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/TM ; 1999-209513
NASA technical memorandum ; 209513.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 2 microfiches.
Added Author
Hunter, Craig A.
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:209513
Research Call Number
READEX Microfiche NAS 1.15:209513
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