Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control / Scott C. Asbury and Craig A. Hunter.
- Physical Description: 1 online resource (134 pages) : illustrations.
- Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 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:||
|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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