| Citation: | HUANG Dao-bo, LI Jian-dong, LIU Yong. Aeroelastic analysis of rotor airfoil based on CFD/CSD tight coupling method[J]. Journal of Aerospace Power, 2016, 31(8): 1820-1829. doi: 10.13224/j.cnki.jasp.2016.08.004 |
| [1] |
Friedmann P P,Hodges D H.Rotary wing aeroelasticity:a historical perspectives[J].Journal of Aircraft,2003,40(6):1019-1046.
|
| [2] |
Bousman W G.Putting the aero back into aeroelasticity[R].NASA/TM-2000-209589,2000.
|
| [3] |
Laxman V,Venkatesan C.Rotor blade dynamic stall model and its influence on airfoil response[R].AIAA-2006-1866,2006.
|
| [4] |
张伟,刘勇.非定常气动模型的多频特研究[C]//第二十五届全国直升机年会论文集.江西景德镇:中国航空学会,2009:341-348.
|
| [5] |
Liu F,Sadeghi M,Yang S,et al.Parallel computation of wing flutter with a coupled Navier-Stokes/CSD method[R].AIAA-2003-1347,2003.
|
| [6] |
Ramji K,Wei S.Fluid-structure interaction for aeroelastic applications[J].Progress in Aerospace Sciences,2004,40(8):535-558.
|
| [7] |
Potsdam M,Yeo H,Johnson W,Rotor airloads prediction using loose aerodynamic/structural coupling[J].Journal of Aircraft,2006,43(3):732-742.
|
| [8] |
Bhagwat M J,Ormiston R A,Saberi H A,et al.Application of CFD/CSD coupling for analysis of rotorcraft airloads and blade loads in maneuvering flight[J].Journal of the American Helicopter Society,2012,57(3):1-21
|
| [9] |
Zaki A A.Using tightly-coupled CFD/CSD simulation rotorcraft stability analysis[D].Atlanta,Georgia:Georgia Institude of Technology,2012.
|
| [10] |
安效民,徐敏,陈士橹.二阶时间精度的CFD/CSD耦合算法研究[J].空气动力学学报,2009,27(5):547-552. AN Xiaomin,XU Min,CHEN Shilu.Analysis for second order time accurate CFD/CSD coupled algorithms[J].Acta Aerodynamic Sinica,2009,27(5):547-552.(in Chinese)
|
| [11] |
谢亮,徐敏,李杰,等.基于CFD/CSD耦合的颤振与动载荷分析方法[J].振动与冲击,2012,31(3):106-110. XIE Liang,XU Min,LI Jie,et al.Flutter and dynamic analysis based on CFD/CSD coupling method[J].Journal of Vibration and Shock,2012,31(3):106-110.(in Chinese)
|
| [12] |
王俊毅,招启军,马砾,等.直升机旋翼桨-涡干扰状态非定常气弹载荷[J].航空动力学报,2015,30(5):1267-1274. WANG Junyi,ZHAO Qijun,MA Li,et al.High-precision prediction on unsteady aeroelastic loads of helicopter rotors under blade-vortex interaction condition[J].Journal of Aerospace Power,2015,30(5):1267-1274.(in Chinese)
|
| [13] |
李建东.基于CFD/CSD耦合的旋翼振动载荷预估方法研究[D].南京:南京航空航天大学,2015. LI Jiandong.Research on rotor vibration load prediction using CFD/CSD coupling[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2015.(in Chinese)
|
| [14] |
Leishman J G,Beddoes T S.A semi-empirical model for dynamic stall[J].Journal of the American Helicopter Society,1989,34(3):3-17.
|
| [15] |
Petot D.Different equation modeling of dynamic stall[R].La Recherche Aerospatiale 1989-5,1989.
|
| [16] |
Truong V K.Prediction of helicopter rotor airloads based on physical modeling of 3-D unsteady aerodynamics[R].Marseiles,France:22nd European Rotorcraft Forum,1972.
|
| [17] |
钱炜棋,符松,蔡金狮.翼型动态失速的数值模拟研究[J].空气动力学学报,2001,19(4):427-432. QIAN Weiqi,FU Song,CAI Jinshi.Numerical study of airfoil dynamic stall[J].Acta Aerodynamic Sinica,2001,19(4):427-432.(in Chinese)
|
| [18] |
McCroskey W J,McAlister K W,Carr L W,et al.An experimental study of dynamic stall on advanced airfoil sections[R].NASA TM-84245,1982.
|