| Citation: | JIANG Xiang-hua, WANG Yan-rong. Numerical simulation of bird impact on bladed rotor stage by fluid-solid coupling method[J]. Journal of Aerospace Power, 2008, 23(2): 299-304.
|
| [1] |
朱俊,李玉龙.飞机鸟撞试验瞬时速度的连续测试方法研究[J].测控技术,2003,22(12):5-7.ZHU Jun,LI Yulong.Research for the instantaneous velocity measurement in aircraft bird-impact test[J].Measurement & Control Technology,2003,22(12):5-7.
|
| [2] |
刘大响,陈光.航空发动机--飞机的心脏[M].北京:航空工业出版社,2003:159-160.
|
| [3] |
Horsley J.The Rolls-Royce way of validating fan integrity[R].AIAA-93-2602,1993.
|
| [4] |
张志林,姚卫星.飞机风挡鸟撞动响应分析方法研究[J].航空学报,2004,25(6):577-580.ZHANG Zhilin,YAO Weixing.Research on dynamic analysis of bird impact on aircraft windshield[J].Acta Aeronautica et Astronautica Sinica,2004,25(6):577-580.
|
| [5] |
武存浩,杨嘉陵,臧曙光,等.鸟撞高速摄影试验与过程研究[J].北京航空航天大学学报,2001,27(3):332-335.WU Cunhao,YANG Jialing,ZHANG Shuguang,et al.Study of bird impact loading model[J].Journal of Beijing University of Aeronautics and Astronautics,2001,27(3):332-335.
|
| [6] |
McCarty R E.MAGNA computer simulation of bird impact on the TF-15 aircraft canopy[R].ADA140701,1983.
|
| [7] |
谢宗蕻,卞文杰,昂海松,等.峰窝夹芯结构雷达罩鸟撞有限元分析与模拟[J].爆炸与冲击,1999,19(3):236-242.XIE Zhonghonga,BIAN Wenjie,AN Haisong,et al.The FEM analysis and simulation of bird impact radome with composite sandwich structure[J].Explosion and Shockwaves,1999,19(3):236-242.
|
| [8] |
姚小虎,韩强,张晓晴,等,飞机圆弧风挡抗鸟撞试验研究[J].爆炸与冲击,2005,25(5):471-422.YAO Xiaohu,HAN Qiang,ZHANG Xiaoqing,et al.Experimental study on arc windshield of fighter subjected to bird Impact[J].Explosion and Shockwaves,2005,25(5):471-422.
|
| [9] |
Audic S,Berthillier M,Bonini J.Prediction of bird impact in hollow fan blades[R].AIAA-2000-3201,2000.
|
| [10] |
Boroughs R R.High speed bird impact analysis of the Learjet 45 windshield using DYNA3D[R].AIAA-98-1705,1998.
|
| [11] |
Stoll F,Brockman R A.Finite element simulation of highspeed soft-body impacts[R].AIAA-97-1093,1997.@[12]Birkbeck J C.Effects of FOD on the fatigue crack initiation of ballistically impacted Ti-6Al-4V simulated engine blades[D].Dayton,Ohio:University of Dayton,2002.8.
|
| [12] |
Birkbeck J C.Effects of FOD on the fatigue crack initiation of ballistically impacted Ti-6Al-4V simulated engine blades[D].Dayton,Ohio:University of Dayton,2002.8.
|
| [13] |
Xi Chen.Foreign object damage and fatigue cracking[D].Cambridge,Massachusetts:Harvard University,2001.5.
|
| [14] |
Boyce B L.Understanding impact-induced fatigue failure[D].USA:University of California,2001.
|
| [15] |
黄志勇,陈伟,赵海欧,等.评定叶片鸟撞击损伤的参数与方法[J].航空发动机,2005,31(1):28-30.HUANG Zhiyong,CHENG Wei,ZHAO Haiou,et al.Parameters and methods for evaluating bird impact damage of fan/compressor blade[J].Aeroengine,2005,31(1):28-30.
|
| [16] |
卞文杰,万力,吴莘馨.瞬态动力学CAE解决方案MSC.Dytran基础教程[M].北京:北京大学出版社,2004,1-15.
|
| [17] |
梁春华.商用飞机发动机几项关键新技术[J].国际航空,2002,(9):53-54.LIANG Chunhua.New technologies used for commercial aircraft engines[J].International Aviation,2002,(9):53-54.
|
DownLoad: