Computational Study of Hypersonic Rarefied Gas Flow over Re-Entry Vehicles Using the Second-Order Boltzmann-Curtiss Constitutive Model
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Publication:5075246
DOI10.1080/10618562.2022.2032680zbMath1487.76052OpenAlexW4293169889MaRDI QIDQ5075246
Vishnu Asokakumar Sreekala, R. S. Myong, T. Chourushi, Satyvir Singh
Publication date: 10 May 2022
Published in: International Journal of Computational Fluid Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1080/10618562.2022.2032680
orthogonal Jacobi polynomialspolynomial approximationtotal dragslip conditionrarefied gas flowdiatomic gasjump conditionmixed discontinuous Galerkin methodtotal heat transfer
Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05) Hypersonic flows (76K05) Basic methods in fluid mechanics (76M99) Diffusive and convective heat and mass transfer, heat flow (80A19) Compressible Navier-Stokes equations (76N06)
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