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Calculation of supersonic flow past wings with consideration of tangential discontinuities shed from the edges within the scope of a model using a system of Euler equations - MaRDI portal

Calculation of supersonic flow past wings with consideration of tangential discontinuities shed from the edges within the scope of a model using a system of Euler equations (Q1147591)

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scientific article; zbMATH DE number 3704218
Language Label Description Also known as
English
Calculation of supersonic flow past wings with consideration of tangential discontinuities shed from the edges within the scope of a model using a system of Euler equations
scientific article; zbMATH DE number 3704218

    Statements

    Calculation of supersonic flow past wings with consideration of tangential discontinuities shed from the edges within the scope of a model using a system of Euler equations (English)
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    1978
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    stationary
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    slender wing
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    tangential discontinuity
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