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

DOI10.1007/BF02698215zbMath0934.76035MaRDI QIDQ1304554

G. N. Dudin

Publication date: 13 April 2000

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

zbMATH Keywords

laminar boundary layerperfect gasstrong viscous-inviscid interactionpower-law shapesemi-infinite thin delta wing

Mathematics Subject Classification ID

Hypersonic flows (76K05)

Related Items (1)

Gas injection from the surface of a triangular plate in a hypersonic flow

Cites Work

• Unnamed Item
• A method of calculating a regime of strong viscous interaction on a delta wing
• Heat transfer at the surface of a triangular body in a hypersonic viscous gas flow
• On the existence of self-similar solutions in the supercritical region on a delta wing in a hypersonic flow
• On the outer-edge problem of a hypersonic boundary layer

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