Performance Analysis of the New Helicopter-Lift Device

Yue Ming Yang; Qin Yu Yang; Jin Bo Yao; Yuan Kai Li

doi:10.4028/www.scientific.net/AMM.380-384.31

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 380-384Performance Analysis of the New Helicopter-Lift...

Performance Analysis of the New Helicopter-Lift Device

Abstract:

Helicopter lift system aerodynamic design is the key to success helicopter design technology. Currently helicopter lift system has complex structure, fuel consumption, low efficiency and many other issues, which greatly limits its potential to play, so the research of new efficient, simple and practical helicopter lift system is imminent. In this paper, a new kind of helicopter-lift device, combined with the whole structure, the specific presentation of the entire lift device works and ways of working. Based on 2D N-S equations and Spalart-Allmaras turbulence model, the device numerical simulation of two-dimensional aerodynamic characteristics. The results showed that: The lift device is feasible, can be applied to the helicopter technology. The results can lift device is designed for the helicopter to provide certain technical reference.

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Periodical:

Applied Mechanics and Materials (Volumes 380-384)

Pages:

31-34

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.380-384.31

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Online since:

August 2013

Authors:

Yue Ming Yang, Qin Yu Yang, Jin Bo Yao, Yuan Kai Li

Keywords:

Aerodynamic Characteristics, Helicopter, Lift Device, Numerical Simulation

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