The commercially available RNG k-e turbulence model with enhanced wall treatment found in Fluent 6.1 was used to solve the flow over a V-22 Osprey wing equipped with blowing slots. The solutions were then compared to experimental data. Good correlation between the computational and experimental data was found. Download on the wing from the rotors while the aircraft is operating in vertical take-off and landing mode was found to be reduced by the blowing slots.
Continued Computational Investigation into Circulation Control for the V-22 Osprey Download Reduction
Sae Technical Papers
Aerospace Technology Conference and Exposition ; 2005
2005-10-03
Aufsatz (Konferenz)
Englisch
Osprey Metals becomes Sandvik Osprey
Emerald Group Publishing | 2005
Online Contents | 1997
|British Library Online Contents | 1997
Online Contents | 2014