Simplified system of equations for calculating the stability of the boundary layer gas flow on a swept wing

DOI10.1134/S001546281404005XzbMath1301.76034OpenAlexW2057392936MaRDI QIDQ477223

S. V. Manuilovich

Publication date: 2 December 2014

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

Full work available at URL: https://doi.org/10.1134/s001546281404005x

zbMATH Keywords

compressible three-dimensional boundary layerTollmien-Schlichting instabilitytransverse flow instability

Mathematics Subject Classification ID

Parallel shear flows in hydrodynamic stability (76E05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Cites Work

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• Stabilization of a laminar boundary layer by an active surface-localized action
• Free interaction of a three-dimensional boundary layer with an exterior irrotational flow
• Receptivity of a high-speed boundary layer to acoustic disturbances

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