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Influence of Lift Offset on Rotorcraft PerformanceThe influence of lift offset on the performance of several rotorcraft configurations is explored. A lift-offset rotor, or advancing blade concept, is a hingeless rotor that can attain good efficiency at high speed by operating with more lift on the advancing side than on the retreating side of the rotor disk. The calculated performance capability of modern-technology coaxial rotors utilizing a lift offset is examined, including rotor performance optimized for hover and high-speed cruise. The ideal induced power loss of coaxial rotors in hover and twin rotors in forward flight is presented. The aerodynamic modeling requirements for performance calculations are evaluated, including wake and drag models for the high-speed flight condition. The influence of configuration on the performance of rotorcraft with lift-offset rotors is explored, considering tandem and side-by-side rotorcraft as well as wing-rotor lift share.
Document ID
20100026468
Document Type
Technical Publication (TP)
Authors
Johnson, Wayne
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 24, 2013
Publication Date
November 1, 2009
Subject Category
Aerodynamics
Report/Patent Number
NASA/TP-2009-215404
ARC-E-DAA-TN717
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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