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Laminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow

S. A. Hosseini؛ S. Noori

دوره 7، شماره 1 ، فروردین 1393، ، صفحه 33-40

چکیده

In the present work, an engineering method is developed to predict laminar and turbulent heating-rate solutions for blunt reentry spacecraft at hypersonic conditions. The calculation of aerodynamic heating around blunt bodies requires alternative solution of inviscid flow field around the hypersonic bodies. In this paper, the procedure is of an inverse nature, that is, a shock wave is assumed and calculations proceed along rays normal to the shock. The solution is iterated until the given body is computed. The inverse method is practical for the calculation of flow field between the shock wave ... بیشتر

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