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V-22 Osprey aerodynamic development — a progress review

Published online by Cambridge University Press:  04 July 2016

M. A. McVeigh ,
J. Liu ,
S. J. O'Toole  and
S. Woods
M. A. McVeigh
Affiliation:
Boeing Defense & Space Group, Helicopters Division Philadelphia, USA
J. Liu
Affiliation:
Boeing Defense & Space Group, Helicopters Division Philadelphia, USA
S. J. O'Toole
Affiliation:
Boeing Defense & Space Group, Helicopters Division Philadelphia, USA
S. Woods
Affiliation:
US Navy
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Abstract

Events in the aerodynamic development of the multi-service V-22 Osprey tiltrotor are reviewed, with emphasis on recent flight test findings and the solutions developed. A discussion of the performance in the USMC, Navy and SOCOM missions is presented.

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 101 , Issue 1006 , July 1997 , pp. 231 - 244
Copyright
Copyright © Royal Aeronautical Society 1997 

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References

1. Rosenstein, H. and Clark, R. Aerodynamic development of the V-22 tiltrotor, AIAA/AHS/ASEE Aircraft Systems Design and Technology Meeting, Dayton, Ohio, October 1986.Google Scholar
2. McVeigh, M.A., Grauer, W.K. and Paisley, D.J. Rotor-airframe interactions, on tiltrotor aircraft, J Ameri Heli Soc, July 1990, 35, (3).Google Scholar
3. Grauer, W.K. and Farrell, M.K. V-22 Flight test aerodynamic, AHS 47th Annual Forum, Phoenix, Arizona, 1991.Google Scholar
4. Savage, M.C., Grauer, W.K., Farrell, M.K. and McVeigh, M.A. . V-22 Flight test aerodynamic refinement, AHS 49th Annual Forum, St Louis, Missouri, 19-21 May 1993.Google Scholar
5. Felker, F.F., Maisel, M.D. and Betzina, M.D. Full scale tiltrotor hover performance, presented at the 41st Annual Forum of the American Helicopter Society, 15-17 May 1985.Google Scholar
6. McVeigh, M.A. The V-22 tiltrotor large scale rotor performance/Wing download test and comparison with theory, 11th European Rotorcraft Forum, London, England, 1985, Paper No 97.Google Scholar
7. Felker, F.F. Results from a test of a 2/3 scale V-22 rotor and wing in the 40 ft by 80 ft windtunnel, 47th Annual Forum of the American Helicopter Society, Phoenix, Arizona, March 1991.Google Scholar
8. Johnson, W. A Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics — CAMRAD, Volumes I & II, User's Manual.Google Scholar
9. McVeigh, M.A., Liu, J. and Wood, T. Aerodynamic development of a forebody strake for the V-22 Osprey, AHS 51st Annual Forum, 9–11 May 1995.Google Scholar
10. Tai, T.C. Simulation and analysis of V-22 rotocraft forward flight flowfield, AIAA paper 95-0046, Aerospace Sciences Meeting, Reno, Nevada, 1995.Google Scholar
11. Buning, p. et al, OVERFLOW Users Manual, Version 1.6ah, July 1993.Google Scholar