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Swirling base injection for supersonic combustion ramjets.Experimental evaluation of the swirling base injection proposed by Swithenbank and Chigier (1969) for application in supersonic combustion ramjets or scramjets. This concept of accelerated mixing in supersonic streams through swirl was tested, but the results indicate that swirl does not produce any enhancement of mixing.
Document ID
19720062119
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Povinelli, L. A.
Ehlers, R. C.
(NASA Lewis Research Center Airbreathing Engines Div., Cleveland, Ohio, United States)
Date Acquired
August 6, 2013
Publication Date
September 1, 1972
Publication Information
Publication: AIAA Journal
Volume: 10
Subject Category
Propulsion Systems
Accession Number
72A45785
Distribution Limits
Public
Copyright
Other

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