Hypersonic viscous gas flow over a delta wing in the intermediate interaction regime with allowance for wake flow

DOI10.1007/BF01050056zbMath0810.76033OpenAlexW2052717505MaRDI QIDQ1339605

G. N. Dudin

Publication date: 6 December 1994

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01050056

zbMATH Keywords

Navier-Stokes equationszero angle of attacksymmetric wake

Mathematics Subject Classification ID

Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10) Hypersonic flows (76K05)

Cites Work

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• Calculation of three-dimensional boundary layer on a triangular plate of finite length in a hypersonic stream
• Three-dimensional boundary layer on a plane delta wing in the intermediate hypersonic interaction regime

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