NASA NTRS · 19720062119
Swirling base injection for supersonic combustion ramjets.
Abstract
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.
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Povinelli, L. A., Ehlers, R. C.. 1972-09-01. Swirling base injection for supersonic combustion ramjets.. https://ntrs.nasa.gov/citations/19720062119
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