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| Structural Dynamical Characteristics of Wing-Engine System with Gyro Effects |
| Zhou Jian-bin1,2, Zhang Jun-jie1, Meng Guang2 |
| 1. Shanghai Aircraft Design and Research Institute of COMAC, Shanghai 200232, P.R. China;2. State Key Laboratory of Mechanical System and Vibration, Shanghai Jiao Tong University, Shanghai 200240, P.R. China |
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Abstract A system of structural dynamical equations of the Bernoulli-Euler cantilever beam with gyro effects was established, using the Hamilton Variant Principle, to simulate the wing-mounted engine/wing system. The me-chanism of coupling effects of the rotor to the structure was analyzed based on the basic theory of gyroscopic mo-ment. The effects of the rotor to the structural dynamical characteristics, with different rotational speeds and struc-tural parameters, were analyzed. This research provided a theoretical foundation for the further study of character-istics of the real wing-engine system, as well as its aeroelastic performance.
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Received: 27 November 2010
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Corresponding Authors:
Zhou Jian-bin
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2012, Vol. 31 
