Conical gas flows with shock waves and turbulent boundary layer separation
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Publication:431761
DOI10.1134/S0015462812020135zbMath1242.76101MaRDI QIDQ431761
A. A. Chulkov, N. A. Ostapenko, M. A. Zubin
Publication date: 2 July 2012
Published in: Fluid Dynamics (Search for Journal in Brave)
boundary layer separationconical flowsMach-type interaction between shock wavessupersonics flowsV-wing
Experimental work for problems pertaining to fluid mechanics (76-05) Shock waves and blast waves in fluid mechanics (76L05) Turbulent boundary layers (76F40) Supersonic flows (76J20)
Related Items (6)
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 ⋮ Structure of supersonic inviscid nonsymmetric conical flow around a V-wing ⋮ On the theory of supersonic inviscid flow separation in gasdynamic problems ⋮ Distinctive features of the shock layer flow structure in conical gas flows
Cites Work
- 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
- Structure of supersonic inviscid nonsymmetric conical flow around a V-wing
- Supersonic flow around a V-shaped wing at incidence and yaw
- Unnamed Item
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