Investigations of XV-15 Rotor Hover Performance and Flow Field Using U2NCLE and HELIOS Codes
Author:
Affiliation:
1. University of Toledo
2. Bell Helicopter Textron, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0303
Reference35 articles.
1. Helf, S. "Full-Scale Hover Test of a 25-Foot Tilt Rotor", BHT Report 300-099-010, NASA CR114626, May 1973.
2. Skin Friction Predictions over a Hovering Tilt-Rotor Blade Using OVERFLOW2
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