Organised modes and shock-vortex interaction in unsteady viscous transonic flows around an aerofoil. II: Reynolds number effect.

DOI10.1016/S0045-7930(02)00101-9zbMath1140.76358OpenAlexW2729143942MaRDI QIDQ1415743

A. Bouhadji, Marianna Braza

Publication date: 9 December 2003

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0045-7930(02)00101-9

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05)

Related Items (1)

Reduced-order modeling of transonic flows around an airfoil submitted to small deformations

Cites Work

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