Numerical simulation of the flow field around a cascade of NACA 0012 airfoils -- effects of solidity and stagger

DOI10.1016/S0045-7825(97)00253-3zbMath0954.76057OpenAlexW2019425464WikidataQ127720488 ScholiaQ127720488MaRDI QIDQ1817815

M. O. Budair, M. Naweed Ahmed, Bekir Sami Yilbas

Publication date: 2 February 2000

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

Full work available at URL: https://doi.org/10.1016/s0045-7825(97)00253-3

zbMATH Keywords

lift\(k\)-epsilon turbulence modeldragflow fieldcontrol volume methodangles of attackmaximum liftcascade of NACA 0012 airfoilsLaplace grid generatortrailing edge separation

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) (k)-(varepsilon) modeling in turbulence (76F60) General aerodynamics and subsonic flows (76G25) Gas dynamics (general theory) (76N15)

Cites Work

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• The calculation of turbulent recirculating flows in general orthogonal coordinates
• Computational study into the flow field developed around a cascade of NACA 0012 airfoils
• Navier-Stokes Solution of the Turbulent Flowfieid about an Isolated Airfoil