Aerodynamic characteristics of a thin airfoil cascade in an ideal incompressible flow with separation from the leading edges

DOI10.1134/S0015462809020021zbMath1213.76034MaRDI QIDQ538952

V. A. Yudin, V. B. Kurzin

Publication date: 26 May 2011

Published in: Fluid Dynamics (Search for Journal in Brave)

zbMATH Keywords

separated flowaerodynamic characteristicscascadeairfoillossesvortex layer

Mathematics Subject Classification ID

Vortex flows for incompressible inviscid fluids (76B47) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (1)

A provably stable and high-order accurate finite difference approximation for the incompressible boundary layer equations

Cites Work

• Using the perturbation method to solve the problem of separated incompressible flow past thin airfoils
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