Abstract

<UMM ARIZE D here are the results of a comprehensive rametric study of the effects of injection of He, C, H2O, Air, Ar, CO2, and Xe into laminar boundary layers at the windwardmost meridians of yawed sharp cones in supersonic streams. Heat-transfer, shear stress, and mass transfer conductance data correlations are obtained. The derived correlation functions are uniformly valid for estimating the effects of foreign gas injection in flows ranging from cones at zero incidence, through windwardmost meridians of yawed sharp cones, to three-dimensional stagnation points.

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