Numerical modeling of three-dimensional vortex structures in hypersonic transverse flow past a cylinder

DOI10.1134/S0015462810050029zbMath1233.76073MaRDI QIDQ665561

S. M. Drozdov

Publication date: 5 March 2012

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

zbMATH Keywords

shock waveshypersonic flowcylindervortex structuresspatial flow periodicity

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Hypersonic flows (76K05)

Related Items (2)

Problem of non-uniqueness of steady-state hypersonic flow past bodies with a cylindrical frontal bluntness ⋮ Experimental modeling of three-dimensional modes of hypersonic flow past cylindrically-blunted bodies

Cites Work

• Vortex structure generation on the frontal surface of a cylinder set transversely in a hypersonic flow
• Effect of compressibility on the development of Taylor-Görtler vortices at high Reynolds numbers
• Receptivity of the blunt-leading-edge plate boundary layer to unsteady vortex perturbations
• Distortion of a flat-plate boundary layer by free-stream vorticity normal to the plate
• Unnamed Item

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