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A summary of wind tunnel research on tilt-rotors from hover to cruise flightAn experimental research program conducted on a series of tilt rotors designed for a range of blades twist is reported. The test facilities used in the program are identified. The objective of the program was to obtain precise results on the influence of blades twist and aeroelasticity on tilt rotor performance from hover to high speed cruise Mach number to 0.7. Five aluminum rigid rotors and one fiber glass composite rotor were tested.
Document ID
19730012322
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Poisson-Quinton, PH. (NASA Ames Research Center Moffett Field, CA, United States)
Cook, W. L. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 7, 2013
Publication Date
February 1, 1973
Publication Information
Publication: AGARD Aerodyn. of Rotary Wings
Subject Category
Aircraft
Accession Number
73N21049
Distribution Limits
Public
Copyright
Other
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