Calculation of radial supersonic gas flow past sharp-nosed cones

Computational Mathematics and Modeling - Tập 7 - Trang 148-159 - 1996
M. G. Lebedev, Yu. N. Sadkov

Tóm tắt

The paper presents the results of numerical analysis of supersonic source flow of a gas past sharp-nosed cones. Axisymmetric and three-dimensional flows are considered. The flow geometry and the distributions of the gas-dynamic parameters in the shock layer are analyzed; their asymptotic properties are established. The numerical solutions are compared with solutions for uniform gas flow past a cone.

Tài liệu tham khảo

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