Rozhdestvenskiy M G, Vaintrub A P.Tilted tail rotor advantages and problems to solve[C]//The 27th European Rotorcraft Forum.Moscow:ERF,1995:1-9
[2]
于雪梅,刘平安, 崔秀娟.用参数辨识法进行直升机悬停性能 拓展[J].航空学报,2010,31(3):466-471 Yu Xuemei,Liu Ping'an,Cui Xiujuan.Helicopter hovering performance expansion by parameter identification[J].Acta Aeronoutica et Astronautica Sinica,2010,31(3):466-471(in Chinese)
[3]
Hilbert K B. A mathematical model of UH-60 helicopter[R].NASA TM85890,1984
[4]
Ostroff A J, Downing D R,Rood W J.A technique using a nonlinear helicopter model for determining trims and derivatives [R].NASA TND8159,1976
[5]
Steiner J, Gandhi F,Yoshizaki Y.An investigation of variable rotor RPM on performance and trim[C]//64th Annual Forum Proceedings of the American Helicopter Society.Montreal:AHS,2008:697-705
Cao Y H. Principles of helicopter flight dynamics[M].Oxfordshire:Coxmoor Publishing Company,2009
[8]
李国知,曹义华. 旋翼结冰对直升机飞行动力学特性的影响[J].航空学报,2011,32(2):187-194 Li Guozhi,Cao Yihua.Effect of rotor icing on helicopter flight dynamics characteristics [J].Acta Aeronoutica et Astronautica Sinica,2011,32(2):187-194(in Chinese)
[9]
徐玉貌,胡士媛, 李杰.尾桨倾斜对直升机飞行性能的影响[J].直升机技术,2008,155(3):82-85 Xu Yumao,Hu Shiyuan,Li Jie.The effect of tail rotor tilting to helicopter's flight performance[J].Helicopter Technique,2008,155(3):82-85(in Chinese)
[10]
王适存. 直升机空气动力学[M].北京:航空专业教材编审组,1985 Wang Shicun.Helicopter aerodynamics[M].Beijing:Aviation Professional Teaching Materials Editing Group,1985(in Chinese)
[11]
曹义华. 直升机飞行力学[M].北京:北京航空航天大学出版社,2005 Cao Yihua.Helicopter flight dynamics [M].Beijing:Beihang University Press,2005(in Chinese)
[12]
Rozhdestvenskiy M G, Vaintrub A P.Tilted tail rotor advantages and problems to solve[C]//The 27th European Rotorcraft Forum.Moscow:ERF,1995:1-9
[13]
Ballin M G. Validation of a real-time engineering simulation of the UH-60A helicopter[R].NASA TM88359,1987
[14]
于雪梅,刘平安, 崔秀娟.用参数辨识法进行直升机悬停性能 拓展[J].航空学报,2010,31(3):466-471 Yu Xuemei,Liu Ping'an,Cui Xiujuan.Helicopter hovering performance expansion by parameter identification[J].Acta Aeronoutica et Astronautica Sinica,2010,31(3):466-471(in Chinese)
[15]
Hilbert K B. A mathematical model of UH-60 helicopter[R].NASA TM85890,1984
[16]
Ostroff A J, Downing D R,Rood W J.A technique using a nonlinear helicopter model for determining trims and derivatives [R].NASA TND8159,1976
[17]
倪先平. 直升机手册[M].北京:航空工业出版社,2003 Ni Xianping.Helicopter handbook[M].Beijing:Aviation Industry Press,2003(in Chinese)
[18]
彭勇, 陈平剑,孙强.斜置尾桨对直升机飞行特性的影响[J].南京航空航天大学学报,2011,43(4):446-452 Peng Yong,Chen Pingjian,Sun Qiang.Effect of canted tail rotor on helicopter flight characteristics[J].Journal of Nanjing University of Aeronautics and Astronautics,2011,43(4):446-452(in Chinese)
[19]
Cao Y H. Principles of helicopter flight dynamics[M].Oxfordshire:Coxmoor Publishing Company,2009
[20]
李国知,曹义华. 旋翼结冰对直升机飞行动力学特性的影响[J].航空学报,2011,32(2):187-194 Li Guozhi,Cao Yihua.Effect of rotor icing on helicopter flight dynamics characteristics [J].Acta Aeronoutica et Astronautica Sinica,2011,32(2):187-194(in Chinese)
[21]
王适存. 直升机空气动力学[M].北京:航空专业教材编审组,1985 Wang Shicun.Helicopter aerodynamics[M].Beijing:Aviation Professional Teaching Materials Editing Group,1985(in Chinese)
[22]
徐玉貌,胡士媛, 李杰.尾桨倾斜对直升机飞行性能的影响[J].直升机技术,2008,155(3):82-85 Xu Yumao,Hu Shiyuan,Li Jie.The effect of tail rotor tilting to helicopter's flight performance[J].Helicopter Technique,2008,155(3):82-85(in Chinese)
[23]
Prouty R W. Should we consider variable rotor speeds[J].Vertiflite,2004,50(4):24-27
[24]
曹义华. 直升机飞行力学[M].北京:北京航空航天大学出版社,2005 Cao Yihua.Helicopter flight dynamics [M].Beijing:Beihang University Press,2005(in Chinese)
[25]
Ballin M G. Validation of a real-time engineering simulation of the UH-60A helicopter[R].NASA TM88359,1987
[26]
倪先平. 直升机手册[M].北京:航空工业出版社,2003 Ni Xianping.Helicopter handbook[M].Beijing:Aviation Industry Press,2003(in Chinese)
[27]
彭勇, 陈平剑,孙强.斜置尾桨对直升机飞行特性的影响[J].南京航空航天大学学报,2011,43(4):446-452 Peng Yong,Chen Pingjian,Sun Qiang.Effect of canted tail rotor on helicopter flight characteristics[J].Journal of Nanjing University of Aeronautics and Astronautics,2011,43(4):446-452(in Chinese)
