Numerical Investigation of Film Coefficient Approximation for Chemically Reacting Boundary-Layer Flows
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DOI: 10.2514/1.t6707
Abstract: Aerothermal analysis of spacecraft planetary entry is heavily dependent on heritage engineering models. The film coefficient heat transfer model examined in this paper estimates the convective heating to the vehicle for a laminar, dissociated, chemically… read more here.
Keywords: chemically reacting; film coefficient; reacting boundary; film ... See more keywords