Some influencing factors of rotor vibratory loads prediction under high speed state

[1] Nixon N W, Yeager W T. Requirements for development of a sequential high-resolution blade and hub loads data set for rotorcraft analysis validation . Presented at the Ninth International Workshop on Aeroelasticity of Rotorcraft Systems . University of Michigan, Ann Arbor, Michigan, 2001 [2] Hansford R E, John W. Dynamics workshop on rotor vibratory loads prediction[J]. Journal of the American Helicopter Society,1998,43(1):76~87 [3] 航空航天工业部科学技术研究院. 直升机动力学手册[M]. 北京:航空工业出版社,1991.49~72 Research Institute of Science Technology of Ministry of Aeronautics and Space Industrial. Helicopter dynamics handbook[M]. Beijing:Aviation Industrial Press,1991.49~72(in Chinese) [4] John W. 直升机理论[M]. 北京:航空工业出版社,1980.91 John W. Helicopter theory[M]. Beijing:Aviation Industrial Press, 1980.91(in Chinese) [5] 辛 宏. 旋翼非定常气动特性的理论和试验研究 . 南京:南京航空航天大学飞行器系,1995 Xin Hong. Theory and experimental research on unsteady aerodynamic characteristics of helicopter rotor . Nanjing:Department of Aircraft, Nanjing University of Aeronautics & Astronautics, 1995(in Chinese) [6] Leishman J G, Beddoes T S. A generalised model for airfoil unsteady Aerodynamic behaviour and dynamic stall using the indicial method . Presented at the 42nd Annual Forum of the American Helicopter Society . Washington D C, 1986.243~265 [7] Johnson W. Development of a comprehensive analysis for rotorcraft-I:rotor model and wake analysis[J]. Vertica,1981,5(2):99~129 [8] He Chengjian. Aeroelasticity and aeromechanics studies in forward flight—an unsteady induced flow theory . United States:School of Aerospace Engineering at Georgia Institute of Technology, 1995 [9] 张晓谷.直升机动力学设计[M]. 北京:航空工业出版社,1995. 35 Zhang Xiaogu. Helicopter dynamics design[M]. Beijing:Aviation Industrial Press,1995.35(in Chinese)