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