Three-dimensional boundary layer on a plane delta wing in the intermediate hypersonic interaction regime

DOI10.1007/BF01059013zbMath0748.76089MaRDI QIDQ1191147

G. N. Dudin

Publication date: 27 September 1992

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

zbMATH Keywords

finite-difference method

Mathematics Subject Classification ID

Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (1)

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

Cites Work

• Unnamed Item
• Calculation of three-dimensional boundary layer on a triangular plate of finite length in a hypersonic stream

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