[1] 李博, 梁德旺, 黄国平. 基于等效盘模型的滑流对涡桨飞机气动性能的影响[J]. 航空学报, 2008, 29(4):845-852. LI B, LIANG D W, HUANG G P. Propeller slipstream effects on aerodynamic performance of turbo-prop airplane based on equivalent actuator disk model[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(4):845-852(in Chinese).[2] 鄂秦, 杨国伟. 螺旋桨滑流对飞机气动特性影响的数值分析[J]. 西北工业大学学报, 1997, 15(4):511-516. E Q, YANG G W. On coupling effect of two vortex systems of Chinese aircraft with turbo-propellers[J]. Journal of Northwestern Polytechnical University, 1997, 15(4):511-516(in Chinese).[3] 夏贞锋, 罗淞, 杨永. 基于激励盘理论的螺旋桨滑流数值模拟研究[J]. 空气动力学学报, 2012, 30(2):219-222. XIA Z F, LUO S, YANG Y. Numerical simulation of propeller slipstream flows using actuator disk theory[J]. Acta Aerodynamica Sinica, 2012, 30(2):219-222(in Chinese).[4] WOLKOVITCH J. The joined wing:An overview[J]. Journal of Aircraft, 1986, 23(3):161-178.[5] 刘学强, 李青, 柴建忠, 等. 盒式机翼布局气动特性研究[J]. 南京航空航天大学学报, 2008, 39(6):722-725. LIU X Q, LI Q, CHAI J Z, et al. Aerodynamic characteristic research for box-wing aircraft[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2008, 39(6):722-725(in Chinese).[6] 李光里, 李国文, 黎军, 等. 连接翼布局气动特性研究[J]. 空气动力学学报, 2006, 24(4):513-519. LI G L, LI G W, LI J, et al. The aerodynamics investi-gation of the joined-wing configuration[J]. Acta Aerodynamica Sinica, 2006, 24(4):513-519(in Chinese).[7] 唐胜景, 刘真畅, 周运强, 等. 后翼上反串置翼无人机气动特性研究[J]. 北京理工大学学报, 2015, 35(12):1211-1216. TANG J S,LIU Z C,ZHOU Y Q, et al. Investigation on aerodynamic performance of tandem wing UAV with rear wing dihedral[J]. Transactions of Beijing Institute of Technology, 2015, 35(12):1211-1216(in Chinese).[8] 王延奎, 单继祥, 田伟, 等. 联翼布局俯仰力矩非线性变化特性的数值模拟[J]. 北京航空航天大学学报, 2012, 38(7):862-866. WANG Y K, SHAN J X, TIAN W, et al. Investigation on non-linear characteristic of pitching moment of joined wing configuration aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(7):862-866(in Chinese).[9] CHANDAR D D J, DAMODARAN M. Computational study of unsteady low-Reynolds number airfoil aerodynamics using moving overlapping meshes[J]. AIAA Journal, 2008, 46(2):429-438.[10] CATALANO F M. On the effects of an installed propeller slipstream on wing aerodynamic characteristics[J]. Acta Polytechnica, 2004, 44(3):8-14.[11] EHAB A E, COLIN P B. Experimental investigation of the effect of propeller slipstream on boundary layer behavior at low Reynolds number:AIAA-2000-4123[R]. Reston, VA:AIAA, 2000.[12] 王科雷, 祝小平, 周洲, 等. 低雷诺数分布式螺旋桨滑流气动影响[J]. 航空学报, 2016, 37(9):2669-2678. WANG K L, ZHU X P, ZHOU Z, et al. A study of distributed electric propulsion slipstream aerodynamic effects at low Reynolds number[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(9):2669-2678(in Chinese).[13] 夏贞锋, 杨永. 螺旋桨滑流与机翼气动干扰的非定常数值模拟[J]. 航空学报, 2011, 32(7):1195-1201. XIA Z F, YANG Y. Unsteady numerical simulation of interaction effects of propeller and wing[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(7):1195-1201(in Chinese).[14] WALTERS D K, COKLJAT D. A three-equation eddy-viscosity model for Reynolds-averaged Navier-Stokes simulations of transitional flow[J]. Journal of Fluids Engineering, 2008, 130(12):1-14.[15] 徐家宽, 白俊强, 黄江涛, 等. 考虑螺旋桨滑流影响的机翼气动优化设计[J]. 航空学报, 2014, 35(11):2910-2920. XU J K, BAI J Q, HUANG J T, et al. Aerodynamic optimization design of wing under the interaction of propeller slipstream[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(11):2910-2920(in Chinese).[16] 陈广强, 白鹏, 詹慧玲, 等. 一种推进式螺旋桨无人机滑流效应影响研究[J]. 空气动力学学报, 2015, 33(4):554-562. CHEN G Q, BAI P, ZHAN H L, et al. Numerical simulation study on propeller slipstream effect on unmanned air vehicle with propeller engine[J]. Acta Aerodynamica Sinica, 2015, 33(4):554-562(in Chinese).[17] GREGORY A W, BRYAN D M, BENJAMIN A B, et al. Summary of low-speed airfoil date-Vol.5[M]. Illinois:University of Illinois at Urbana-Champaign, 2012.[18] KONING C. Influence of the propeller on other parts of the airplane structure[M]//Aerodynamic Theory. Berlin Heidelberg:Springer, 1935:402-420.[19] 刘沛清, 王亚平, 刘杰, 等. 近距耦合鸭式布局复杂涡系的干扰机理[J]. 北京航空航天大学学报, 2012, 38(7):873-881. LIU P Q, WANG Y P, LIU J, et al. Vortex interaction mechanism over close-coupled canard configuration[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(7):873-881(in Chinese).[20] 马宝峰, 刘沛清, 邓学蓥. 近距耦合鸭式布局气动研究进展[J]. 空气动力学学报, 2003, 21(3):320-329. MA B F, LIU P Q, DENG X Y. Research advances on a close-coupled canard wing configuration[J]. Acta Aero-dynamica Sinica, 2003, 21(3):320-329(in Chinese).[21] 段中喆, 刘沛清. 某型螺旋桨滑流对机翼气动性能影响的数值研究[J]. 应用基础与工程科学学报, 2012(S1):215-225. DUAN Z J, LIU P Q. Numerical researches on the aerodynamic characteristics of a wing influenced by the slipstream of propellers[J]. Journal of Basic Science and Engineering, 2012(S1):215-225(in Chinese).