Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air
By: W.I. Scallion.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 104097.
Publisher: National Aeronautics and Space Administration, Langley Research Center; For sale by the National Technical Information Service
Published: 1991
Place of publication: Hamtpon, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Nozzle design.; Nozzle geometry.; Plumes.; Pressure ratio.; Shapes.; Supersonic nozzles.
Notes: Also available via Internet from the NASA Technical Report Server web site. Address as of 4/26/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910014816%5F1991014816.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991]. 1 microfiche.