谭湘霞, 吴斌, 余旭东, 等. 导弹折叠翼的机构弹性动力学分析与仿真 研究[J]. 弹箭与制导学报, 1999(1): 17-21. Tan Xiangxia, Wu Bin, Yu Xudong, et al. Elastic dynamics analysis and simulation research of missile folding wing[J]. Journal of Projectiles Rockets Missiles and Guidance, 1999(1): 17-21.
[2]
王党校. 飞行器折叠机构弹性动力分析[D]. 西安: 西北工业大学, 2000. Wang Dangxiao. Elastic dynamic analysis of aircraft folding mechanism[D]. Xi'an: Northwestern Polytechnical University, 2000.
[3]
王仲华. 飞行器折叠尾翼的弹性动力学有限元数值分析[D]. 西安: 西 北工业大学, 2004. Wang Zhonghua. Elastic dynamic FEM numerial analysis of aerocraft folded-wing[D]. Xi'an: Northwestern Polytechnical University, 2004.
[4]
思灿勇. 重型直升机尾桨动力学特性与动响应分析[D]. 南京: 南京航 空航天大学, 2010. Si Canyong. Dynamic properties and responses of heavy-lift helicopter tail rotor[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2010.
[5]
魏来. 基于多体动力学的直升机动部件综合系统动特性分析[D]. 南 京: 南京航空航天大学, 2011. Wei Lai. Research on dynamic characteristic analysis of helicopter dynamic component comprehensive system based on dynamics of multibody[ D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2011.
[6]
贺天鹏, 李书, 张俊, 等. 共轴式直升机双旋翼系统的多体动力学模型[J]. 振动、测试与诊断, 2013, 33(增1): 91-96. He Tianpeng, Li Shu, Zhang Jun, et al. Multibody dynamics model of coaxial helicopter rotor system[J]. Journal of Vibration, Measurement & Diagnosis, 2013, 33(Suppl 1): 91-96.
[7]
普劳蒂R W. 直升机性能及操纵性和稳定性[M]. 北京: 航空工业出版 社, 1990. Prouty R W. Helicopter performance, stability and control[M]. Beijing: Aviation Industry Press, 1990.