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Continued Computational Investigation into Circulation Control for the V-22 Osprey Download Reduction
ISSN: 0148-7191, e-ISSN: 2688-3627
Published October 3, 2005 by SAE International in United States
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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.
- Brian M. O’Hara - Center for Industrial Research Applications (CIRA), West Virginia University
- Gerald M. Angle - Center for Industrial Research Applications (CIRA), West Virginia University
- Wade W. Huebsch - Center for Industrial Research Applications (CIRA), West Virginia University
- James E. Smith - Center for Industrial Research Applications (CIRA), West Virginia University
CitationO’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.
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