Structure of supersonic inviscid nonsymmetric conical flow around a V-wing

DOI10.1134/S0015462811040132zbMath1233.76072MaRDI QIDQ665648

N. A. Ostapenko, M. A. Zubin, A. A. Chulkov

Publication date: 5 March 2012

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

zbMATH Keywords

supersonic flowsconical flowsV-wingMach interaction between shock waves

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Supersonic flows (76J20)

Related Items (4)

Inviscid vortex structures in the shock layers of conical flows around V wings ⋮ Conditions of the existence of vortex ferri singularities in supersonic conical flows ⋮ Conical gas flows with shock waves and turbulent boundary layer separation ⋮ Distinctive features of the shock layer flow structure in conical gas flows

Cites Work

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• Conical gas flows with shock waves and turbulent boundary layer separation
• Submerged shocks in conical gas flows in the presence of a Mach shock-wave configuration
• Calculation of supersonic flow around V-shaped wings by the fitting method
• Hypersonic flow past an airfoil with a Mach system of shock waves
• Supersonic flow around a V-shaped wing at incidence and yaw
• Hypersonic flow past delta wing of finite thickness

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