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《Journal of Nanjing University of Aeronautics & Astronautics》 1992-01
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Effect of Different Force-Functions and Initial Shock Pressure on Blade Response

Yin Jing Li Qinghong (Department of Power Engineering)  
The effect of two kinds of load factors of bird impact on blade response is analysed in this paper. They are the force-functions and the initial shock pressure. The finite element method is used to compute the nonlinear transient response of the cantilever plate by means of simulating a real blade with a rectangular cantilever plate and simulating bird impact loads with shock loads. The conclusions obtained in this paper may provide references for the development of the bird impact load model.
【Fund】: 航空科学基金
【CateGory Index】: V232. 4;;V214. 43
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Chinese Journal Full-text Database 1 Hits
1 Yin Jing,Gao Deping,Fan Erning (Nanjing University of Aeronautics and Astronautics);LOADING MODELS FOR BIRD IMPACTING ON BLADES[J];Journal of Aerospace Power;1993-04
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1 WU Cun hao YANG Jialing (Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics) ZANG Shu guang MA Juan rong (China Building Materials Academy);Study of Bird Impact Loading Model[J];Journal of Beijing University of Aeronautics and Astronautics;2001-03
2 ;Bird Ingestion into Aero-Engine and Resolved Methods[J];International Aviation;1996-10
3 Gao Deping [WT5HX](Nanjing Aeronautical Institute) [WT5HZ]Li Qinghong [WT5HX](China Estern Airlines);ANALYTICAL AND EXPERIMENTAL INVESTIGATION OF BIRD IMPACT ON BLADES[J];Journal of Aerospace Power;1990-04
4 Yin Jing(Nanjing Aeronautical Institute);EFFECT OF SOME LOAD FACTORS OF BIRD IMPACT ON BLADE RESPONSE[J];Journal of Aerospace Power;1992-01
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7 Chen Wei,Qi Wenkai,Gao Deping(2nd Dept.Nanjing University of Aeronautics and Astronautics,Nanjing 210016);TRANSIENT RESPONSES OF BLADES TO BIRD IMPACT COUPLED WITH DEFORMATIONS OF BLADE[J];JOURNAL OF AEROSPACE POWER;1998-01
8 Huang Zhiyong 1 Chen Wei 1 Zhao Hai′ou 1 Yan chenghong 2(1. Nanjing University of Aeronautics and Astronautics, Nanjing 210016,China)(2. China Civil Aviation Flight College, Guanghan 618307,China);Parameters and Methods for Evaluating Bird Impact Damage of Fan/Compressor Blade[J];Aeroengine;2005-01
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【Secondary References】
Chinese Journal Full-text Database 6 Hits
1 WANG Fu-sheng1,YUE Zhu-feng1,FENG Zhen-zhou2,WANG Xin-jun3(1.School of Mechanics Civil Engineering and Architecture,Northwestern Polytechnical University,Xi′an 710072,China)(2.AVICⅠThe First Aircraft Institute,Xi′an 710089,China)(3.Nuclear Power Institute of China,Chengdu 610041,China);Present Study Status of Numerical Simulation Methods of Dynamic Response for Aircraft Windshield under Bird Strike[J];Aircraft Design;2008-05
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