Continued Computational Investigation Into Circulation Control for the V-22 Osprey Download Reduction

Document Number: 2005-01-3187

Date Published: October 2005

Author(s):
Brian O'Hara - West Virginia Univ.
Gerald M. Angle - West Virginia Univ.
Wade W. Huebsch - West Virginia Univ.
James Smith - West Virginia Univ

Abstract:
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.

File Size: 785K
Product Status: In Stock

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