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- W2948839285 abstract "The future development trend of helicopter will possess the function of high speed, far distance and high ceiling. Now, the main development trend of compound helicopters at home and abroad are the conventional configuration with auxiliary propulsion unit and the wing. But for this configuration, the force on the parts are very different from the ordinary. To solve this problem, it need to ensure the allocation of the lift between rotor and wing in the stage of general design. In this paper, for Rotor/wing compound helicopter, build a calculation model of required power and put up a kind of lift distribution strategy between the rotor and the wing and analyze it in different flight status. Through the research, the project of lift distribution has been confirmed. At the same time, to improve the working efficiency of the propellers, build an optimization model to modify propellers geometric parameters in I-sight. According to the optimized parameters, the working efficiency of the propellers have been verified to promote a lot." @default.
- W2948839285 created "2019-06-14" @default.
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- W2948839285 date "2019-01-01" @default.
- W2948839285 modified "2023-10-17" @default.
- W2948839285 title "The Optimization Design of Lift Distribution and Propeller Performance for Rotor/Wing Compound Helicopter" @default.
- W2948839285 doi "https://doi.org/10.1007/978-981-13-3305-7_87" @default.
- W2948839285 hasPublicationYear "2019" @default.
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