[1] Jenney D S. ABCTM aircraft development status[C]//6th European Rotorcraft and Powered Lift Aircraft Forum. Bristol: University of Bristol, 1980: 27-47.[2] Ruddell A J. Advancing blade concept(ABCTM) development[C]//32th Annual National V/STOL Forum of the American Helicopter Society, 1976: 71-82.[3] Ruddell A J, Macrino J A. Advancing blade concept(ABCTM) high speed development[C]//36th Annual National Forum of the American Helicopter Society, 1980: 1-13.[4] Fort F F. Performance and loads data from a wind tunnel test of a full-scale, coaxial, hingeless rotor helicopter, NASA-TM-81329[R]. Washington, D. C.: NASA, 1981.[5] Robert K B. The ABCTM rotor-a history perspective[C]//62nd Annual Forum of the American Helicopter Society, 2004: 1-47.[6] Blackwell R, Millott T. Dynamics design characteristics of the sikorsky X2 technologyTM demonstrator aircraft[C]//64th Annual Forum of the American Helicopter Society, 2008: 1-13.[7] Walsh D, Weiner S, Arifian K, et al. High airspeed testing of the sikorsky X2 technology demonstrator[C]//67th Annual Forum of the American Helicopter Society International, 2011: 1-17.[8] Bagai A. Aerodynamic design of the X2 technology demonstrator main rotor blade[C]//64th Annual Forum of the American Helicopter Society, 2008: 1-16.[9] Kim H W, Kenyon A R, Duraisamy K, et al. Interactional aerodynamics and acoustics propeller-augmented compound coaxial helicopter[C]//American Helicopter Society Specialists Conference on Aeromechanics. San Francisco:University of Strathclyde, 2008: 1-22.[10] Potsdam M, Yeo H, Johnson W. Rotor airloads prediction using loose aerodynamic/structural coupling[J]. Journal of Aircraft, 2006, 43(3): 732-742.[11] Jung S N, Sa J H, You Y H, et al. Loose fluid-structure coupled approach for a rotor in descent incorporating fuselage effects[J]. Journal of Aircraft, 2013, 50(4): 1016-1026.[12] Pahlke K, van der Wall B G.Chimera simulations of multibladed rotors in high-speed forward flight with weak fluid-structure-coupling[J]. Aerospace Science and Technology, 2005, 9(5): 379-389.[13] Hodges D H, Dowell E H. Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades, NASA TN D-7818[R]. Washington, D. C.: NASA, 1974.[14] Jia D W. Study on some aeroelastic and stability analyses of tiltrotor[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2007. (in Chinese) 贾大伟. 倾转旋翼机气弹响应及稳定性若干问题研究[D]. 南京: 南京航空航天大学, 2007.[15] Yang A M, Qiao Z D. Navior -Stokes computation for a helicopter rotor in forword flight based on moving overset grids[J]. Acta Aeronautica et Astronautica Sinica, 2001, 22(5): 434-436. (in Chinese) 杨爱明, 乔志德. 基于运动嵌套网格的前飞旋翼绕流N-S方程数值计算[J]. 航空学报, 2001, 22(5): 434-436.[16] Tian S L, Wu Y Z, Xia J. Numerical simulation research of unsteady flow field around helicopter in forward flight on dynamic overset unstructured grids[J]. Acta Aeronautica et Astronautica Sinica, 2007, 28(5): 1047-1054. (in Chinese) 田书玲, 伍贻兆, 夏健. 基于动态非结构重叠网格法的直升机前飞非定常流场数值模拟研究[J]. 航空学报, 2007, 28(5): 1047-1054. |