Problem of non-uniqueness of steady-state hypersonic flow past bodies with a cylindrical frontal bluntness

DOI10.1134/S0015462814020057zbMath1294.76191OpenAlexW2000679907MaRDI QIDQ404044

S. M. Drozdov

Publication date: 29 August 2014

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

Full work available at URL: https://doi.org/10.1134/s0015462814020057

zbMATH Keywords

shock wavehypersonic flowsvortex structurecylinderflow mode non-uniqueness

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Hypersonic flows (76K05)

Uses Software

• FLUENT

Cites Work

• Vortex structure generation on the frontal surface of a cylinder set transversely in a hypersonic flow
• Numerical modeling of three-dimensional vortex structures in hypersonic transverse flow past a cylinder
• Effect of compressibility on the development of Taylor-Görtler vortices at high Reynolds numbers

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