Citation: | XIANG Jin-wu, GUO Jun-xian, ZHANG Xiao-guet al. An Overview of Rotor Blades Optimum Design for Helicopter Vibration Reduction[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(1): 32-35. (in Chinese) |
[1] 张晓谷. 直升机动力学设计[M]. 北京:航空工业出版社,1995.1~6. [2] Gabel R.When helicopter smooth surpasses jet smooth-keynote address. In:Specialists Meeting on Helicopter Vibration. Hartford:American Helicopter Society,1981. 1~10. [3] Friedman P P.Application of modern structural optimization methods to vibration reduction in rotorcraft[J]. Vertica,1985, 9(4):363~376. [4] Peters D A,Rossow M P,Korn A,et al. Design of helicopter rotor blades for optimum dynamic characteristics[J]. Journal of Compt & Math with Appl, 1986,12(1):85~109. [5] 程耿东,顾元宪,候汝良,等.旋翼桨叶的频率敏度分析与调频及优化设计[J].直升机技术, 1983,3(3):21~39. [6] 向锦武,张呈林,王适存.低振动旋翼桨叶的动力学优化设计[J].航空动力学报,1996,11(2):125~128. [7] Taylor R B. Helicopter vibration reduction by rotor blade modal shaping. In: Proceedings of the 38th Annual Forum. Maryland:American Helicopter Society, 1982. 223~229. [8] Pritchard J I, Adelman H M. Optimal placement of tuning masses for vibration reduction in helicopter rotor blades[J]. AIAA Journal,1990, 28(2):233~239. [9] Bennett R L. Optimum structural design. In:Proceedings of the 38th Annual Forum. Maryland:American Helicopter Society,1982. 121~129. [10] Straub F K,Callahan C B,Culp J D.Rotor design optimization using a multidisciplinary approach[J].Journal of Structural Optimization, 1992, 5(1-2):70~75. [11] Hodges D H,Dowell E H. Nonlinear equations of motion for elastic bending and torsion of twisted non-uniform blades. NASA-TN-D-7818,1974. [12] Rosen A,Friedmann P P. Nonlinear equations of equilibrium for elastic helicopter or wind turbine blades undergoing moderate deformation. UCLA-ENG-7718,1977. [13] Refield L W. Design analysis methodology for composite rotor blades. AFWAL-TR-85-3094, 1985. [14] Giavotto V,Borri M. Anisotropic beam theory and applications[J]. Computer & Structure, 1983,16(1-4):403~413. [15] 向锦武,张晓谷,赵 翔. 直升机旋翼桨叶剖面刚度的有限元计算[J].航空动力学报,1998,13(2):206~208. [16] Hodges D H. A mixed variational formulation based on exact intrinsic equations for dynamics of moving beam[J]. International Journal of Solids and Structures, 1990,26(11):1253~1273. [17] Friedmann P P, Shanthakumaran P. Optimum design of rotor blades for vibration reduction in forward flight[J]. Journal of American Helicopter Society,1984, 29(4):334~342. [18] Kim K C, Chopra I. Aeroelastic analysis of helicopter rotor blades with advanced tip shapes. AIAA-No-1118, 1990. [19] Ganguli R, Chopra I. Aeroelastic optimization of a helicopter rotor to reduce vibration and dynamic stresses[J].Journal of Aircraft, 1996, 12(4):334~342. [20] Bielawa R L. Techniques for stability analysis and design optimization with dynamic constraints on non-conservative linear systems. In:Proceedings of the 12th AIAA/ASME/ SSDM Conference. Maryland:AIAA/ASM, 1971.334~327. [21] Miura H. Application of numerical optimization methods to helicopter design problems-a survey[J]. Vertica, 1985,9(2):141~154. [22] Davis M W, Weller W H. Applications of design optimization techniques to rotor dynamics problems[J]. Journal of American Helicopter Society,1988,33(3):42~50. [23] Adelman H M, Mantay W R. Integrated multidisciplinary design optimization of rotorcraft[J]. Journal of Aircraft,1991, 28(1):67~77. [24] Lim J W, Chopra I. Aeroelastic optimization of helicopter rotor using an efficient sensitivity analysis[J]. Journal of Aircraft,1991, 28(1):123~129. [25] Straub F K, Ealey M A, Schelky L McD. Application of smart material to helicopter rotor active control. A97-3160508-31,1997. [26] Nagashima T. The state of the art of active control technology for helicopter vibration reduction (survey). A96-3287508-31,1995.
|