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Computational Study of Hypersonic Rarefied Gas Flow over Re-Entry Vehicles Using the Second-Order Boltzmann-Curtiss Constitutive Model - MaRDI portal

Computational Study of Hypersonic Rarefied Gas Flow over Re-Entry Vehicles Using the Second-Order Boltzmann-Curtiss Constitutive Model (Q5075246)

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scientific article; zbMATH DE number 7524850
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Computational Study of Hypersonic Rarefied Gas Flow over Re-Entry Vehicles Using the Second-Order Boltzmann-Curtiss Constitutive Model
scientific article; zbMATH DE number 7524850

    Statements

    Computational Study of Hypersonic Rarefied Gas Flow over Re-Entry Vehicles Using the Second-Order Boltzmann-Curtiss Constitutive Model (English)
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    10 May 2022
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    rarefied gas flow
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    mixed discontinuous Galerkin method
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    polynomial approximation
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    orthogonal Jacobi polynomials
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    diatomic gas
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    slip condition
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    jump condition
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    total drag
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    total heat transfer
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