Submerged shocks in conical gas flows in the presence of a Mach shock-wave configuration

DOI10.1134/S0015462807020160zbMath1200.76118MaRDI QIDQ605839

A. A. Chulkov, N. A. Ostapenko

Publication date: 25 November 2010

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

zbMATH Keywords

supersonic flowconical flowsMach interaction of shocksV-wings

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

Related Items (2)

Conical gas flows with shock waves and turbulent boundary layer separation ⋮ Structure of supersonic inviscid nonsymmetric conical flow around a V-wing

Cites Work

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• Calculation of supersonic flow around V-shaped wings by the fitting method
• Supersonic flow around a V-shaped wing at incidence and yaw
• Nonlinear conical flow of a gas

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