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Calculation of the maximum hypersonic fineness ratio and optimal configuration of short-span wings with laminar and turbulent boundary layers. - MaRDI portal

Calculation of the maximum hypersonic fineness ratio and optimal configuration of short-span wings with laminar and turbulent boundary layers. (Q1569385)

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scientific article; zbMATH DE number 1467910
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English
Calculation of the maximum hypersonic fineness ratio and optimal configuration of short-span wings with laminar and turbulent boundary layers.
scientific article; zbMATH DE number 1467910

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    Calculation of the maximum hypersonic fineness ratio and optimal configuration of short-span wings with laminar and turbulent boundary layers. (English)
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    4 July 2000
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    In the paper a new method combining analytical and numerical approaches is applied to calculate the electric field in a gas laser. It is shown that the method guarantees efficient and highly accurate calculation of the strength of a strongly nonuniform electric field inside the computational domain up to the segments of the domain boundary with a rapidly varying boundary curvature. A model problem of optimization of the shape of electrodes is solved. Numerical results are presented.
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