Copyright © A. Filippone (1997-1999-2004). All Rights Reserved.

Low Aspect-Ratio Wings


Below is an example of state-of-the-art Navier-Stokes computations using a multi-grid multi-block solver for a high Reynolds number flow a planar wing of aspect-ratio 1. Re=3 million, angle of attack=- 0 deg.



Wing AR=1, top streamlines



Wing AR=1, bottom streamlines



Wing AR=1, VSAERO



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Copyright © A. Filippone (1997-1999-2004). All Rights Reserved.