1926. Tilt Rotor Wing Weight Estimation

Publication TypeConference Paper
AuthorsSchmidt, A.H.; Dyess, S.B.
Year of Publication1990
Paper Number1926
Conference49th Annual Conference, Chandler, Arizona, May 14-16
Conference LocationChandler, Arizona
Paper Category23. WEIGHT ENGINEERING - STRUCTURAL ESTIMATION
Pages34
Date Published5/14/90
Price$13.60
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Key Words23. WEIGHT ENGINEERING - STRUCTURAL ESTIMATION
AbstractThe wing of a tilt rotor aircraft has some design requirements which differ from that of conventional aircraft. The bending moment due to lifting the aircraft at the wing tips is larger than that of normal wing lift loads, and the natural frequency of the wing must be kept separated from the rotor one per rev. This paper presents a method, based on composite construction, for tilt rotor wing weight estimation.