Inviscid vortex structures in the shock layers of conical flows around V wings

DOI10.1134/S0015462817030115zbMath1370.76081OpenAlexW2645040628MaRDI QIDQ2402756

N. A. Ostapenko, F. A. Maksimov, M. A. Zubin

Publication date: 14 September 2017

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

Full work available at URL: https://doi.org/10.1134/s0015462817030115

zbMATH Keywords

shock wavelambda shock wave configurationsupersonic conical flowturbulent boundary layer separationV wingvortex Ferri singularity

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Turbulent boundary layers (76F40) Supersonic flows (76J20)

Related Items (1)

The mode of attached compression shock at edges of a V-shaped wing

Cites Work

• Conical gas flows with shock waves and turbulent boundary layer separation
• Structure of supersonic inviscid nonsymmetric conical flow around a V-wing
• Conditions of the existence of vortex ferri singularities in supersonic conical flows

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