Interacting flow theory and trailing edge separation – no stall
DOI10.1017/S0022112083001305zbMath0541.76045MaRDI QIDQ3328996
Publication date: 1983
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
wakecatastrophic stallwindward differencingsubsonic or supersonicFinite difference approximationsthin airfoilsComputed stream line patternscondensed problem of two such layersirregularities on discontinuitiesnon- symmetric trailing edge flowsone-sided separationpressure-displacement relationtriple-deck approach of three layerstwo-dimensional, steady-state, laminar boundary layer equations
Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10) Basic methods in fluid mechanics (76M99)
Related Items (7)
Cites Work
- Triple-deck solutions for subsonic flow past humps, steps, concave or convex corners and wedged trailing edges
- The influence of airfoil thickness and Reynolds number on separation
- The interaction of a shock wave with a laminar boundary layer
- The blowhard problem - inviscid flows with surface injection
- Marginal Separation
- D’Alembert’s Paradox
- The numerical solution of the asymptotic equations of trailing edge flow
- Starting vortex, separation bubbles and stall: a numerical study of laminar unsteady flow around an airfoil
- Numerical and asymptotic solutions for the supersonic flow near the trailing edge of a flat plate at incidence
- Self-induced interactions
- Trailing-edge stall
- Boundary-Layer Flow Near the Trailing Edge of a Flat Plate
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