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Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control / Scott C. Asbury and Craig A. Hunter.

Record details

  • Physical Description: 1 online resource (134 pages) : illustrations.
  • Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 1999.

Content descriptions

General Note: "August 1999."
"Performing organization: NASA Langley Research Center"--Report documentation page.
Bibliography, etc. Note: Includes bibliographical references (pages 19-20).
Type of Report and Period Covered Note: Technical memorandum.
Funding Information Note: Sponsored by the National Aeronautics and Space Administration WU 538-14-12-01 L-17879
Source of Description Note: Description based on online resource; title from PDF title page (NASA, viewed Sep. 6, 2017).

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