Parallel computation of flows around flapping airfoils in biplane configuration

2002-05-22
Unsteady, laminar flows over flapping airfoils in biplane configuration are computed on overset grids. The overset grid solutions are obtained in parallel in a cluster environment. It is shown that airfoils in biplane configuration and oscillating in pitch and plunge with a proper phase shift between them enhance the thrust production significantly.

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Citation Formats
İ. H. Tuncer and M. Ç. Kaya, “Parallel computation of flows around flapping airfoils in biplane configuration,” 2002, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/30808.