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This paper presents an experimental investigation to study the effect of injecting a secondary jet of slot width, t, into the main stream of a zero pressure gradient, two dimensional flow parallel to a flat test surface. The injection angle (α) to the downstream of the main flow direction (x) varies from 30 o to 90 o . The study covers a blowing ratio (M) range of 1.5 to 4.2. Tests...
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