Continued Computational Investigation into Circulation Control for the V-22 Osprey Download Reduction 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.
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, https://doi.org/10.4271/2005-01-3187. Download Citation
Author(s):
Brian M. O’Hara, Gerald M. Angle, Wade W. Huebsch, James E. Smith
Affiliated:
Center for Industrial Research Applications (CIRA), West Virginia University
Pages: 9
Event:
Aerospace Technology Conference and Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
SAE 2005 Transactions Journal of Aerospace-V114-1
Related Topics:
Vertical take-off and landing (VTOL)
Wind tunnel tests
Propellers and rotors
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