SEPARATED FLOW STUDIES AT HYPERSONIC SPEEDS. PART II. TWO-DIMENSIONAL WEDGE SEPARATED FLOW STUDIES,
CORNELL AERONAUTICAL LAB INC BUFFALO N Y
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The paper describes an experimental study of the flow patterns and distribution of heat transfer developed in regions of adverse pressure gradient and separated flow over two-dimensional models. The investigation was directed towards obtaining information on two basic problems, the separation and the reattachment of a laminar boundary layer.