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On mathematical modeling of a hypersonic flow past a thin wing with variable shape - MaRDI portal

On mathematical modeling of a hypersonic flow past a thin wing with variable shape (Q2668901)

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On mathematical modeling of a hypersonic flow past a thin wing with variable shape
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    On mathematical modeling of a hypersonic flow past a thin wing with variable shape (English)
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    9 March 2022
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    small parameter
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    integro-differential equation
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    Euler-Ampère transform
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    asymptotic solution
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    semi-inverse method: thin shock-layer method
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