Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air /

Bibliographic Details
Main Author:	Scallion, W. I.
Corporate Author:	Langley Research Center
Format:	Government Document Book
Language:	English
Published:	Hamtpon, Va. : National Aeronautics and Space Administration, Langley Research Center : [1991]
Series:	NASA technical memorandum ; 104097.
Subjects:	Nozzle design. Nozzle geometry. Plumes. Pressure ratio. Shapes. Supersonic nozzles.
Online Access:	https://purl.fdlp.gov/GPO/LPS60070

Description
Item Description:	Microform.
Physical Description:	1 volume 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.