Effect of a hump on the stability of subsonic boundary layers over an airfoil

DOI10.1016/0020-7225(95)00126-3zbMath0900.76122OpenAlexW1979101426MaRDI QIDQ1386045

H. T. Abu-Khajeel, Ali Hasan Nayfeh

Publication date: 2 August 1998

Published in: International Journal of Engineering Science (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0020-7225(95)00126-3

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Parallel shear flows in hydrodynamic stability (76E05)

Related Items (4)

Linear and non-linear stability analysis of incompressible boundary layer over a two-dimensional hump ⋮ A local scattering approach for the effects of abrupt changes on boundary-layer instability and transition: a finite-Reynolds-number formulation for isolated distortions ⋮ Influence of two-dimensional smooth humps on linear and non-linear instability of a supersonic boundary layer ⋮ A local scattering theory for the effects of isolated roughness on boundary-layer instability and transition: transmission coefficient as an eigenvalue

Cites Work

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• Effect of wall cooling on the stability of compressible subsonic flows over smooth humps and backward-facing steps
• Subharmonic instability of compressible boundary layers
• Effect of suction on the stability of subsonic flows over smooth backward-facing steps
• Scattering of acoustic waves into Tollmien-Schlichting waves by small streamwise variations in surface geometry
• Localized receptivity of boundary layers
• Laminar flow control of subsonic boundary layers by suction and heat-transfer strips
• A numerical study of the interaction between unsteay free-stream disturbances and localized variations in surface geometry
• Acoustic receptivity of a boundary layer to Tollmien–Schlichting waves resulting from a finite-height hump at finite Reynolds numbers

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