Copyright © A. Filippone (1996-2001). All Rights Reserved.
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Navier-Stokes Computations



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 past a helicopter fuselage. Data: Re=30 million, angle of attack=- 5 deg.



Helicopter Fuselage



Streamlines



Streamlines at tail

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Copyright © A. Filippone (1996-2001). All Rights Reserved.