Effect of wall cooling on the stability of compressible subsonic flows over smooth humps and backward-facing steps

DOI10.1063/1.857788zbMath0704.76028OpenAlexW2022638734MaRDI QIDQ3484533

A. A. Al-Maaitah, Saad A. Ragab, Ali Hasan Nayfeh

Publication date: 1990

Published in: Physics of Fluids A: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1063/1.857788

zbMATH Keywords

subsonic flowswall coolingtwo-dimensional linear stabilityflows over smooth humpsshear-layer instabilitytwo- dimensional surface

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Hydrodynamic stability (76E99) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10)

Related Items (4)

Linear and non-linear stability analysis of incompressible boundary layer over a two-dimensional hump ⋮ Transition prediction and control in subsonic flow over a hump ⋮ Effect of a hump on the stability of subsonic boundary layers over an airfoil ⋮ Influence of two-dimensional smooth humps on linear and non-linear instability of a supersonic boundary layer

Cites Work

• Nonparallel stability of heated two-dimensional boundary layers
• Computational Solution of Linear Two-Point Boundary Value Problems via Orthonormalization
• Stability of Plane Poiseuille Flow with Heat Transfer

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