Heat transfer at the surface of a triangular body in a hypersonic viscous gas flow

DOI10.1007/BF01051549zbMath0664.76074MaRDI QIDQ1115724

G. N. Dudin

Publication date: 1988

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

zbMATH Keywords

boundary layerthree-dimensional boundary layerviscous interactionexternal hypersonic flowflow divergencesemi-infinite triangular body of power-law shape

Mathematics Subject Classification ID

Gas dynamics (general theory) (76N15) Hypersonic flows (76K05) Basic methods in fluid mechanics (76M99)

Related Items (1)

Influence of intense surface cooling on hypersonic viscous flow past a delta wing

Cites Work

• Unnamed Item
• A method of calculating a regime of strong viscous interaction on a delta wing
• On the outer-edge problem of a hypersonic boundary layer

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