Adaptive CFD analysis for rotorcraft aerodynamics

DOI10.1016/S0045-7825(99)00368-0zbMath1004.76050MaRDI QIDQ1588037

Mark S. Shephard, Mustafa Dindar, Joseph E. Flaherty, Kenneth E. Jansen

Publication date: 6 February 2003

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

zbMATH Keywords

adaptive finite element methodmesh refinementinterpolation errorerror indicatorvortex tubesrotor-blade aerodynamicsvortex core detection

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) General theory of rotating fluids (76U05) Finite element methods applied to problems in fluid mechanics (76M10) Parallel numerical computation (65Y05)

Related Items (1)

Universal meshes for smooth surfaces with no boundary in three dimensions

Cites Work

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• Flowfield of a lifting rotor in hover - A Navier-Stokes simulation
• Automatic three‐dimensional mesh generation by the finite octree technique
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