Singularities of the flow field in the neighborhood of the windward surface of a small aspect ratio delta wing in hypersonic stream

DOI10.1134/S0015462821050037zbMath1478.76047OpenAlexW3202509743MaRDI QIDQ2052750

V. N. Golubkin

Publication date: 26 November 2021

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

Full work available at URL: https://doi.org/10.1134/s0015462821050037

zbMATH Keywords

concentrated forceentropy layerattached shock wavedetached shock waveasymptotic thin shock layer methodsingular cross-section

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Asymptotic methods, singular perturbations applied to problems in fluid mechanics (76M45) Hypersonic flows (76K05)

Cites Work

• Three-dimensional hypersonic gas flow over wings
• Recent Hypersonic Studies of Wings and Bodies
• Thickness effect on the force of slender delta wings in hypersonic flow
• LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY
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