An inviscid model of unsteady aerofoil flow with fixed upper surface separation

DOI10.1002/FLD.1650050607zbMath0568.76019OpenAlexW2082963423MaRDI QIDQ3685405

R. A. Mcd. Galbraith, Marco Vezza

Publication date: 1985

Published in: International Journal for Numerical Methods in Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/fld.1650050607

zbMATH Keywords

wakeunsteady separationseparating shear layershelicopter rotorsDiscrete vorticestwo-dimensional aerofoilvortex panels

Mathematics Subject Classification ID

Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10) Basic methods in fluid mechanics (76M99)

Related Items (1)

Simulation of the flow past a circular cylinder using an unsteady panel method

Cites Work

• Vorticity and Kutta Condition for Unsteady Multienergy Flows

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