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

DOI10.1134/S0015462819030030zbMath1428.76091OpenAlexW2970740930WikidataQ127279979 ScholiaQ127279979MaRDI QIDQ2281952

A. V. Ledovskij, G. N. Dudin

Publication date: 6 January 2020

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

Full work available at URL: https://doi.org/10.1134/s0015462819030030

zbMATH Keywords

asymptotic methodboundary layerdelta wingstrong hypersonic interaction

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Asymptotic methods, singular perturbations applied to problems in fluid mechanics (76M45) Viscous-inviscid interaction for compressible fluids and gas dynamics (76N17) Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Cites Work

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• Flow past a delta wing in the strong viscous-inviscid interaction regime
• Heat transfer in the neighborhood of a point of injection in the leading edge of a plate in hypersonic flight
• A NON-UNIQUENESS OF THE HYPERSONIC BOUNDARY LAYER
• On three-dimensional hypersonic flow fast slender airfoils

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