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Calculation of Two-Dimensional Inlet Flow Fields by an Implicit Method Including Viscous Effects:Program Documentation and Test Case.

机译:用包含粘性效应的隐式方法计算二维入口流场:程序文档和测试用例。

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摘要

The source listing of a computer code for calculating the flow fields in a supersonic free stream is given. The application of this code to an inlet on an airbreathing missile is also presented.

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