TU BRAUNSCHWEIG
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Workgroup Aerodynamics of Aircraft
Prof. Dr.-Ing. R. Radespiel

Computed pressure distribution on the surface of a megaliner

 

Computed flow at the fuselage-empennage junction

     

Hypersonic flow around a generic flap model

 

Analysis of flapping wing flight by numerical flow computation


last changed 2008-05-17 Druckversion
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Responsible: Prof. Dr.-Ing. R. Radespiel
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