Formation of supercritical flow regions on low-aspect-ratio wings

DOI10.1007/S10697-006-0012-4zbMath1198.76113OpenAlexW2033763232MaRDI QIDQ604428

G. N. Dudin

Publication date: 10 November 2010

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

Full work available at URL: https://doi.org/10.1007/s10697-006-0012-4

zbMATH Keywords

boundary layerhypersonic flowdelta wingstrong interaction

Mathematics Subject Classification ID

Viscous-inviscid interaction for compressible fluids and gas dynamics (76N17) Hypersonic flows (76K05)

Related Items (1)

Propagation of perturbations in the three-dimensional boundary layer on a delta wing in the viscid-inviscid interaction regime

Cites Work

• Unnamed Item
• Law of transverse sections for the three-dimensional boundary layer on a thin wing in a hypersonic stream
• On the existence of self-similar solutions in the supercritical region on a delta wing in a hypersonic flow
• A limiting solution for flow past a delta wing in the presence of supercritical flow regions

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