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Factors which influence the analysis and design of ejector nozzlesA theoretical analysis of the viscous interaction between the primary and secondary streams of ejector nozzles was developed. The analysis accounts for real sonic line effects and the streamwise variation in stream mixing and boundary layer within the ejector. The aspects of the analysis are explained and illustrated by applying the theory to a variety of ejector configurations including cylindrical shroud, contoured flap and plug nozzles. Extensive comparisons are made between theory and data to show the importance of various analytical assumptions and such design variables as diameter ratio, spacing ratio, total temperature ratio, and primary nozzle geometry.
Document ID
19720006652
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, B. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
E-6698
NASA-TM-X-67976
Report Number: E-6698
Report Number: NASA-TM-X-67976
Meeting Information
Meeting: Aerospace Sci. Meeting
Location: San Diego, CA
Country: United States
Start Date: January 17, 1972
End Date: January 19, 1972
Accession Number
72N14301
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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