| [1]BENO E A.Analysis of helicopter maneuver-loads and rotor loads flight test data[R]. NASA CR-2225, March 1973.[2]SCHILLINGS J J, ROBERTS B J, WOOD T L.Maneuver performance comparison between the XV15 and an advanced tiltrotor design[J].JAHS, 1990, 35(2):4-14[3]BHAGWAT M J, ORMISTON R A, SABERI H A.Application of CFD/CSD coupling for analysis of rotorcraft airloads and blade loads in maneuvering flight.[J].,[J].Proceedings of the 63rd Annual Forum of the American Helicopter Society, 2007, 1(1):1-13[4]BHAGWAT M J, ORMISTON R A.Examination of rotor aerodynamics 30 in steady and maneuvering flight using CFD and conventional methods[C]// American Helicopter Society Specialist' s Conference on Aeromechanics, San Francisco, CA, anuary 3-25, 2008.[5]ABHISHEK A, DATTA A, ANANTHAN S.Prediction and analysis of main rotor loads in a prescribed pull-up maneuver[J].Journal of Aircraft, 2010, 47(4):1197-1215[6]ABHISHEK A, ANANTHAN S, BAEDER J, et al.Prediction and fundamental understanding of stall loads in UH-60A pull-up maneuver[C]// American Helicopter Society 66th Annual Forum and Technology Display, Phoenix, Arizona, May 11–13, 2010.[7]ABHISHEK A, SILBAUGH B, ANANTHAN S, et al.Coupled CFD/CSD analysis of a prescribed pull-up maneuver[C]// 3rd International Basic Research Conference on Rotorcraft Technology, Nanjing, China, Oct. 14–16, 2009.[8]RAJMOHAN N.Application of hybrid methodology to rotors in steady and maneuvering flight[D]. Ph.D. Thesis, School of Aerospace Engineering, Georgia Inst. of Technology, Atlanta, GA, 2010.[9]辛宏.旋翼非定常气动特性的理论和试验研究[D]. 南京: 南京航空航天大学航空宇航学院, 1995.[10]林永峰, 陈文轩, 邓建军.旋翼非定常气动载荷实验研究[J].南京航空航天大学学报, 2003, 35(3):404-307[11]王芳.机动飞行状态下的旋翼入流和响应分析[D]. 南京: 南京航空航天大学, 2008.[12]吴伟.直升机飞行动力学模型辨识与机动飞行研究[D]. 南京: 南京航空航天大学, 2010.[13]李攀, 陈仁良.直升机急拉杆机动飞行仿真建模与验证[J].航空学报, 2010, 31(12):2315-2323[14]刘勇, 邵松, 朱清华, 等.基于时间精确自由尾迹方法的旋翼非定常气动特性分析[J].航空学报, 2012, 33(4):607-616[15]王亮权.旋翼桨-涡干扰的数值模拟及机动飞行噪声研究[D]. 南京: 南京航空航天大学, 2018.[16]DATTA A, SITARMAN J, CHOPRA I, et al.CFDCSD prediction of rotor vibratory loads in high-speed flight[J].Journal of Aircraft, 2006, 43(6):1698-1709[17]赵国庆, 招启军, 吴琪.旋翼非定常气动特性模拟的通用运动嵌套网格方法[J].航空动力学报, 2015, 30(3):546-554[18]印智昭, 招启军, 王博.基于高阶格式的旋翼非定常涡流场数值模拟[J].航空学报, 2016, 37(08):2552-2564[19]HE T.A partitioned implicit coupling strategy for incompressible flow past an oscillating cylinder[J].International Journal of Computational Methods, 2015, 12(2):1550012-1550025[20]HAMADE K S, KUFELD R M.Modal analysis of uh-60a instrumented rotor blades[R], NASA-TM-4239, 1990.[21]SITARAMAN J, BAEDER J, CHOPRA I.Validation of UH-60A rotor blade aerodynamic characteristics using CFD[C]// American Helicopter Society 59th Annual Forum, Phoenix: AHS, 2003: 42-58.[22]ANUBHAV D.Fundamental understanding, prediction and validation of rotor vibratory loads in steady level flight[D]. Prince George' s County, Maryland: University of Maryland, 2004. |