Flow past a delta wing in the strong viscous-inviscid interaction regime

DOI10.1134/S0015462815040079zbMath1325.76156OpenAlexW1181667524MaRDI QIDQ893582

F. H. Nguen, G. N. Dudin

Publication date: 19 November 2015

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

Full work available at URL: https://doi.org/10.1134/s0015462815040079

zbMATH Keywords

matchingboundary layerdelta wingstrong interaction

Mathematics Subject Classification ID

Viscous-inviscid interaction for compressible fluids and gas dynamics (76N17) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (1)

Distinctive features of flow in the hypersonic boundary layer in the vicinity of the plane of symmetry of a planar wing having a bend of the leading edge

Cites Work

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• A method of calculating a regime of strong viscous interaction on a delta wing
• Law of transverse sections for the three-dimensional boundary layer on a thin wing in a hypersonic stream
• On three-dimensional hypersonic flow fast slender airfoils

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