Supersonic Two-Dimensional Jet-Interaction Studies
Description:
Abstract: The report describes the results of an experimental study involving the injection of a gaseous secondary jet into an unbounded supersonic flow field which was uniform outside of a turbulent boundary layer. The investigation was principally concerned with the formulation of the shock wave shapes and streamline patterns to be associated with typical turbulent, two-dimensional jet-interaction flows. In support of this objective, results are presented for a Mach 5 test conducted using a f…
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Date:
December 17, 1970
Creator:
Werle, Michael J.; Driftmyer, Richard T. & Shaffer, David G.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department