Correlated unsteady and steady laminar trailing-edge flows

DOI10.1017/S0022112081002061zbMath0469.76012MaRDI QIDQ3923772

No author found.

Publication date: 1981

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

zbMATH Keywords

momentsliftaerofoil stallflow near trailing edgeoscillating aerofoilviscous correction to Kutta condition

Mathematics Subject Classification ID

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)

Related Items (3)

Separated supersonic flow past a trailing edge at incidence ⋮ The effect of small surface perturbations on the pulsatile boundary layer on a semi-infinite flat plate ⋮ Viscous extension of potential-flow unsteady aerodynamics: the lift frequency response problem

Cites Work

• On the viscous flow about the trailing edge of a rapidly oscillating plate
• Trailing-edge stall
• Boundary-Layer Flow Near the Trailing Edge of a Flat Plate

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