Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control
By: Scott C. Asbury and Craig A. Hunter.
Contributors: Hunter, Craig A.; Langley Research Center.
Series: NASA/TM -- 1999-209513.; NASA technical memorandum -- 209513.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Exhaust nozzles.; Porosity.; Hole geometry (Mechanics); Cavities.; Thrust vector control.
Other titles: Static performance of a fixed geometry exhaust nozzle incorporating porous cavities for shock boundary layer interaction control.
Notes: Shipping list no.: 2000-0197-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 2 microfiches.