Computational Investigation of a Full-Scale Proprotor Hover Performance and Flow Transition
Author:
Affiliation:
1. University of Toledo, Toledo, Ohio 43606
2. Bell Helicopter Textron Inc., Fort Worth, Texas 76118
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034015
Reference25 articles.
1. MaiselM. D.GiulianettiD. J.DuganD. C. “The History of the XV-15 Tilt Rotor Research Aircraft,” NASA SP-2000-4517, 2000.
2. “Advancement of Proprotor Technology: Wind-Tunnel Test Results Task II,” NASA CR-114363, 1971.
3. FelkerF. F.BetzinaM. D.SignorD. B. “Performance and Loads Data from a Hover Test of a Full-Scale XV-15 Rotor,” NASA TM-86833, 1985.
4. Skin Friction Measurements on a Hovering Full-Scale Tilt Rotor
5. Skin-Friction Predictions on a Hovering Tilt-Rotor Blade
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