Continued Computational Investigation into Circulation Control for the V-22 Osprey Download Reduction
Date Published: 2005-10-03
Paper Number:2005-01-3187
DOI: 10.4271/2005-01-3187
Citation:
O’Hara, B., Angle, G., Huebsch, W., and Smith, J., "Continued Computational Investigation into Circulation Control for the V-22 Osprey Download Reduction," SAE Technical Paper 2005-01-3187, 2005, doi:10.4271/2005-01-3187.
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.
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Product Status: In Stock
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