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The general analysis of Part 1 is applied to the calculation of the second-order viscous and thermal boundary layers for the axisymmetric stagnation point, unsymmetric plane stagnation point, and cusped leading edge at ideal incidence. The second-order effect upon heat transfer is found usually to be of the order of one-third of that for skin friction.
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Milton Van Dyke (1962) studied this question.
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