Continued Computational Investigation into Circulation Control for the V-22 Osprey Download Reduction Center for Industrial Research Applications (CIRA), West Virginia University

Format:

Conference/Event

Author/Creator:

OHara, Brian M., author.

Conference Name:

Aerospace Technology Conference & Exposition (2005-10-03 : Grapevine, Texas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 2005

Summary:

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

Notes:

Vendor supplied data

Publisher Number:

2005-01-3187

Access Restriction:

Restricted for use by site license