Abstract
Theme T purpose of this paper is to present a simple method for predicting heat transfer on the leeward symmetric plane of a blunted body at a moderate angle of attack. The energy integral for the laminar boundary layer on a plane of symmetry provides a qualitative explanation of the increase of heat transfer in a separated flow region. Using the locally similar solutions of the laminar boundary-layer equation, heat transfer is correlated with the inviscid flow parameters at the boundary-layer edge. This correlation equation was testified by comparing with experimental data for a yawed blunt cone in a hypersonic flow.
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