Abstract

Subsequent investigations, in particular of the heat transfer, would be useful in establishing the extent to which approximate methods such as the one considered herein agree with more exact solutions or experimental results. It is of note that the calculation of the heat transfer to the wall is less clear, there being numerous specifications, i.e., by being consistent with that obtained from the similarity solutions, by using the similarity solutions directly with p as the parameter,' by using the integral form of the energy equation, or by other methods suggested for the one parameter method e.g., Hays and Probstein and Chan, but there is little heat transfer data to appraise the various methods in flows over a large range of speeds and accelerations such as in supersonic nozzles.

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