[1] |
LEISHMAN J G.Principles of helicopter aerodynamics[M].2nd ed.New York:Cambridge University Press,2006:658-682.
|
[2] |
LEONI R D.Black hawk:The story of a world class helicopter[M].Reston:AIAA,2007:88-102.
|
[3] |
PROUTY R W,AMER K B.The YAH-64 empennage and tail rotor-a technical history[C]//38th American Helicopter Society Annual Forum.Fairfax,VA:AHS,1982:247-261.
|
[4] |
MAIN B J,MUSSI F.EH101-development status report[C]//Proceedings of the 16th European Rotorcraft Forum.Glasgow:ERF,1990:Ⅲ.2.1.1-12.
|
[5] |
EGLIN P.Aerodynamic design of the NH90 helicopter stabilizer[C]//Proceedings of the 23rd European Rotorcraft Forum.Glasgow:ERF,1997:68.1-68.10.
|
[6] |
朱宇,张宏林,刘莉.直升机低速飞行特性试验分析[J].航空工程进展,2012,3(4):433-437.ZHU Y,ZHANG H L,LIU L.Flight test research on helicopter low speed flight characteristics[J].Advances in Aeronautical Science and Engineering,2012,3(4):433-437(in Chinese).
|
[7] |
TALBOT P D,TINLING B E,DECKER W A,et al.A mathematical model of a single main rotor helicopter for piloted simulation:NASA TM-84281[R].Moffett Field:NASA,1982.
|
[8] |
HE C,LEWIS W D.A parametric study of real time mathematical modeling incorporating dynamic wake and elastic blades[C]//Proceedings of the 48th Annual Forum of the American Helicopter Society.Fairfax,VA:AHS,1992:1181-1196.
|
[9] |
陈仁良.直升机飞行动力学数学建模及机动性研究[D].南京:南京航空航天大学,1998:25-56.CHEN R L.Helicopter flight dynamics mathematical modeling and maneuvering research[D].Nanjing:Nanjing University of Aeronautics and Astronautics,1998:25-56(in Chinese).
|
[10] |
曹义华.直升机机动飞行旋翼的气动力模拟[J].航空学报,1999,20(1):39-42.CAO Y H.Modeling the aerodynamic force of a maneuvering helicopter rotor[J].Acta Aeronautica et Astronautica Sinica,1999,20(1):39-42(in Chinese).
|
[11] |
THEODORE C R.Helicopter flight dynamics simulation with refined aerodynamic modeling[D].College Park,Maryland:University of Maryland,2000:35-105.
|
[12] |
SPOLDI S,RUCKEL P.High fidelity helicopter simulation using free wake,lifting line tail,and blade element tail rotor models[C]//Proceedings of the 59th Annual Forum of the American Helicopter Society.Fairfax,VA:AHS,2003:92-99.
|
[13] |
李攀.旋翼非定常自由尾迹及高置信度直升机飞行力学建模研究[D].南京:南京航空航天大学,2010:14-58.LI P.Rotor unsteady free-vortex wake model and investigation on high-fidelity modeling of helicopter flight dynamics[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2010:14-58(in Chinese).
|
[14] |
GANGWANI S T.Calculation of rotor wake induced empennage airloads[J].Journal of the American Helicopter Society,1983,28(2):37-46.
|
[15] |
CURTISS H C,QUACKENBUSH T R.The influence of the rotor wake on rotorcraft stability and control[C]//15th European Rotorcraft Forum.Glasgow:ERF,1989:70.1-70.24.
|
[16] |
FLETCHER T M,BROWN R E.Main rotor-empennage interaction and its effects on helicopter flight dynamics[C]//Proceedings of the American Helicopter Society 63rd Annual Forum.Fairfax,VA:AHS,2007:1-11.
|
[17] |
WANG B,ZHAO Q J,XU G H,et al.Numerical analysis on noise of rotor with unconventional blade tips based on CFD/Kirchhoff method[J].Chinese Journal of Aeronautics,2013,26(3):572-582.
|
[18] |
KOMERATH N M,SMITH M J,TUNG C.A review of rotor wake physics and modeling[J].Journal of the American Helicopter Society,2011,56(2):022006-1-21.
|
[19] |
HE C J,ZHAO J G.Modeling rotor wake dynamics with viscous vortex particle method[J].AIAA Journal,2009,47(4):902-915.
|
[20] |
魏鹏,史勇杰,徐国华,等.基于粘性涡模型的旋翼流场数值方法研究[J].航空学报,2011,33(5):771-780.WEI P,SHI Y J,XU G H,et al.Numerical method for simulating rotor flow field based upon viscous vortex model[J].Acta Aeronautica et Astronautica Sinica,2011,33(5):771-780(in Chinese).
|
[21] |
TAN J F,WANG H W.Simulating unsteady aerodynamics of helicopter rotor with panel/viscous vortex particle method[J].Aerospace Science and Technology,2013,30(1):255-268.
|
[22] |
谭剑锋,王浩文,吴超,等.基于非定常面元/黏性涡粒子混合法的旋翼/平尾非定常气动干扰研究[J].航空学报,2014,35(3):643-656.TAN J F,WANG H W,WU C,et al.Rotor/empennage unsteady aerodynamic interaction with unsteady panel/viscous vortex particle hybrid method[J].Acta Aeronautica et Astronautica Sinica,2014,35(3):643-656(in Chinese).
|
[23] |
谭剑锋.直升机旋翼对尾桨非定常气动载荷的影响[J].航空学报,2015,36(10):3228-3240.TAN J F.Influence of helicopter rotor on tail rotor unsteady aerodynamic loads[J].Acta Aeronauica et Astronautica Sinica,2015,36(10):3228-3240(in Chinese).
|
[24] |
吴超,谭剑锋,王浩文,等.基于GA/LM混合优化的直升机全机配平算法[J].飞行力学,2014,32(1):5-19.WU C,TAN J F,WANG H W,et al.Optimal trim for helicopter based on GA and LM hybrid algorithm[J].Flight Dynamics,2014,32(1):5-19(in Chinese).
|
[25] |
CROSS J,BRILLA J,KUFELD R,et al.The modern rotor aerodynamic limits survey:A report and data survey:NASA TM-4446[R].Moffett Field:NASA,1993.
|
[26] |
倪先平.直升机手册[M].北京:航空工业出版社,2003:65-68.NI X P.Manual of helicopter[M].Beijing:Aviation Industry Press,2003:65-68(in Chinese).
|