Numerical solutions for oscillatory aerofoil at high reduced frequency

DOI10.1016/0045-7825(89)90086-8zbMath0687.76005OpenAlexW1997274074MaRDI QIDQ1263388

K. Appert

Publication date: 1989

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7825(89)90086-8

zbMATH Keywords

liftKutta conditiondragpressure distributiontrailing edgeunsteady motionpitching momentinviscid incompressible flownonlinear wake effectthick symmetrical Von Mises aerofoil oscillationtwo dimensional aerofoilunsteady aerodynamic propertiesvortex wake pattern

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)

Numerical simulation of unsteady transonic flows using a field integral equation method

Cites Work

• Investigation of numerical solutions of integral equation methods for multi-element aerofoils
• Vorticity and Kutta Condition for Unsteady Multienergy Flows

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