[1] 昌敏,周洲,郑志成.太阳能飞机原理及总体参数敏度分析[J].西北工业大学学报,2010,28(5):792-796.CHANG M,ZHOU Z,ZHENG Z C.Flight principles of solar-powered airplane and sensitivity of its conceptual parameters[J]. Journal of Northwestern Polytechnical University,2010,28(5):792-796(in Chinese). [2] 邓海强,余雄庆.太阳能飞机的现状和发展趋势[J].航空科学技术, 2006(1):28-30.DENG H Q,YU X Q.Solar aircraft:Status and directions[J]. Aeronautical Science and Technology,2006(1):28-30(in Chinese). [3] 刘强,刘强,白鹏,等.不同雷诺数下翼型气动特性及层流分离现象演化[J].航空学报,2017,38(4):22-34.LIU Q,LIU Q,BAI P,et al.Aerodynamic characteristics of airfoil and evolution of laminar separation at different Reynolds numbers[J].Acta Aeronautica et Astronautica Sinica,2017,38(4):22-34(in Chinese). [4] 甘文彪,周洲,许晓平.仿生全翼式太阳能无人机气动数值模拟[J]. 航空学报,2015,36(10):3284-3294.GAN W B,ZHOU Z,XU X P.Aerodynamic numerical simulation of bionic full-wing typical solar-powered unmanned aerial vehicle[J]. Acta Aeronautica et Astronautica Sinica,2015,36(10):3284-3294(in Chinese). [5] NOLL T E,BROWN J M,PEREZ-DAVIS M E,et al.Investigation of the Helios prototype aircraft mishap.Volume I.Mishap report[R].Washington, D.C.:NASA, 2004. [6] 王伟,周洲,祝小平,等.考虑几何非线性效应的大柔性太阳能无人机静气动弹性分析[J].西北工业大学学报,2014,32(4):499-504.WANG W,ZHOU Z,ZHU X P,et al.Static aeroelastic characteristics analysis of a very flexible solar powered UAV with geometrical effect considered[J].Journal of Northwestern Polytechnical University,2014,32(4):499-504(in Chinese). [7] DILLSAVER M J,CESNIK C E S,KOLMANOVSKY I V.Gust response sensitivity characteristics of very flexible aircraft[C]//AIAA Atmospheric Flight Mechanics Conference.Reston:AIAA,2012:1-20. [8] CHARLE T,GREGORY S.Comparsion of computation and experimental studies for a joined wing aircraft:AIAA-2002-0702[R].Reston:AIAA,2002. [9] LEDOUX S,VASSBERG J,FATTA G,et al.Aerodynamic cruise design of a joined wing sensorcraft:AIAA-2008-7190[R].Reston:AIAA,2008. [10] 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 aerodynamic investigation of the joined-wing configuration[J].Acta Aerodynamica Sinica,2006,24(4):513-519(in Chinese). [11] 吴光辉,王妙香,张健.盒式布局飞机的纵向气动参数优化研究[J].飞行力学,2007,25(4):5-7.WU G H,WANG M X,ZHANG J.Research on longitudinal aerodynamic parameter optimize of a joined-wing configuration aircraft[J].Flight Dynamics,2007,25(4):5-7(in Chinese). [12] CATALANO F M.On the effects of an installed propeller slipstream on wing aerodynamic characteristics[J].Acta Polytechnica,2004,44(3):8-14. [13] 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). [14] 王红波,祝小平,周洲,等.基于非定常面元/黏性涡粒子法的低雷诺数滑流气动干扰[J].航空学报,2017,38(4):120412.WANG H B,ZHU X P,ZHOU Z,et al.Aerodynamic interactions at low Reynolds number slipstream with unsteady panel/viscous vortex particle method[J].Acta Aeronautica et Astronautica Sinica,2017,38(4):120412(in Chinese). [15] RAJAGOPALAN R G,LIM C K.Laminar flow analysis of a rotor in hover[J].Journal of the American Helicopter Society,1991,36(1):12-23. [16] ZORI L A J,RAJAGOPALAN R G. Navier-Stokes calculations of rotor-airframe interaction in forward flight[J].Journal of the American Helicopter Society,1995,40(2):57-67. [17] O'BRIEN M,SMITH M J.Analysis of rotor-fuselage interactions using various rotor models:AIAA-2005-468[R].Reston:AIAA, 2005. [18] 宋长红,林永峰,陈文轩,等.基于动量源方法的涵道尾桨CFD分析[J].直升机技术,2009(1):6-11.SONG C H,LIN Y F,CHEN W X,et al.CFD analysis for the ducted tail rotor based on momentum-source method[J].Helicopter Technique,2009(1):6-11(in Chinese). [19] 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):320-327. [20] LYON C A,BROEREN A P,GIGUERE P,et al.Summary of low-speed airfoil data-Vol.3[M].Virginia Beach:Soartech Publications,1997:279-286. |