Calculation of three-dimensional boundary layer on the leeward side of a delta wing of finite length in the hypersonic flow in viscous interaction regime

DOI10.1007/BF01052093zbMath0798.76078MaRDI QIDQ1317699

G. N. Dudin

Publication date: 12 April 1994

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

zbMATH Keywords

boundary value problemwakepressure distributionsubcritical flowsmall angle of attack

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Cites Work

• Unnamed Item
• Calculation of three-dimensional boundary layer on a triangular plate of finite length in a hypersonic stream
• On the outer-edge problem of a hypersonic boundary layer