Computation of attached flow past an airfoil profile at high Reynolds numbers

DOI10.1016/0021-8928(90)90138-ZzbMath0737.76017OpenAlexW2010418054MaRDI QIDQ1180896

S. A. Velichko, Yu. B. Lifshits

Publication date: 27 June 1992

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(90)90138-z

zbMATH Keywords

incompressible fluidturbulent boundary layerwakeeffect of viscositytrailing edgeaerodynamic characteristicsairfoilChaplygin-Zhukovskij 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 (1)

Numerical simulation of viscous transonic flows over an airfoil

Cites Work

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• Laminar separation
• Numerical simulation of viscous transonic flows over an airfoil
• The law of the wake in the turbulent boundary layer
• On displacement thickness
• Trailing-edge stall
• Vortex computation by the method of weighted residuals using exponentials

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