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An experimental study supporting the development of an analytical model for jet-interaction-induced separation of supersonic turbulent boundary layers is discussed. Extensive flat-plate tests were conducted at a Mach number of four and two Reynolds numbers. Surface pressures were recorded fore and aft of the four, sonic, normal jet slots tested. Shadowgraphs, taken through glass-ported side plates, were made of both the interacting and freejet plume characteristics. Generalized correlations showed that the entire problem scales directly with the observed shock heights and that these shock heights are predictable from freejet considerations.
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Werle et al. (1972) studied this question.
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