Unsteady Navier-Stokes solutions for a NACA 0012 airfoil

DOI10.1016/S0045-7825(99)00107-3zbMath0965.76054MaRDI QIDQ1574288

P. S. Murthy, V. S. Holla, Hemant Kamath

Publication date: 29 July 2001

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

zbMATH Keywords

liftNACA 0012 airfoilangle of attackdragsecond-order central difference schemeviscous fluxesbody-fitted curvilinear coordinate O-grid systemfinite volume implicit schemeinviscid fluxesthird-order Roe's schemeunsteady compressible Navier-Stokes equations

Mathematics Subject Classification ID

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

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