[1] 朱自强, 王晓璐, 吴宗成, 等.民机的一种新型布局形式:翼身融合体飞机[J].航空学报, 2008, 29(1):49-59. ZHU Z Q, WANG X L, WU Z C, et al.A new type of transport-blended wing body aircraft[J].Acta Aeronautica et Astronautica Sinica, 2008, 29(1):49-59(in Chinese).
[2] 张帅, 夏明, 钟伯文.民用飞机气动布局发展演变及其技术影响因素[J].航空学报, 2016, 37(1):30-44. ZHANG S, XIA M, ZHONG B W.Evolution and technical factors influencing civil aircraft aerodynamic configuration[J].Acta Aeronautica et Astronautica Sinica, 2016, 37(1):30-44(in Chinese).
[3] 孙占久, 刘龙, 李华, 等.飞翼布局无人机气动/隐身综合性能分析[J].飞行力学, 2018, 36(3):15-18, 27. SUN Z J, LIU L, LI H, et al.Analysis on aerodynamic/stealth synthetical performance of flying wing UAV[J].Flight Dynamics, 2018, 36(3):15-18, 27(in Chinese).
[4] 姚军锴, 曹德一, 何海波.飞翼布局飞行器舵面缝隙对操纵效率的影响[J].空气动力学学报, 2017, 35(6):850-854. YAO J K, CAO D Y, HE H B.Gap influence on rudder efficiency of flying wing aircraft[J].Acta Aerodynamica Sinica, 2017, 35(6):850-854(in Chinese).
[5] WILDSCHEK A.Flight dynamics and control related challenges for design of a commercial blended wing body aircraft[C]//AIAA Guidance, Navigation, and Control Conference.Reston:AIAA, 2014.
[6] 张同鑫, 赵轲, 李权.飞翼布局无人机腹襟翼气动设计研究[J].空气动力学学报, 2019, 37(1):75-82. ZHANG T X, ZHAO K, LI Q.Aerodynamic design of belly-flap for flying wing unmanned aircraft[J].Acta Aerodynamica Sinica, 2019, 37(1):75-82(in Chinese).
[7] STAELENS Y, BLACKWELDER R, PAGE M.Study of belly-flaps to enhance lift-and pitching moment coefficient of a BWB-airplane[C]//25th AIAA Applied Aerodynamics Conference.Reston:AIAA, 2007.
[8] 陈曦.高超声速飞机水平起飞腹部襟翼增升方案研究[D].长沙:国防科技大学, 2017:33-41. CHEN X.Research of the belly flap lift-enhancement scheme of the hypersonic aircraft horizontal take-off[D].Changsha:National University of Defense Technology, 2017:33-41(in Chinese).
[9] STAELENS Y, BLACKWELDER R, PAGE M.Novel pitch control effectors for a blended wing body airplane in takeoff and landing configuration[C]//45th AIAA Aerospace Sciences Meeting and Exhibit.Reston:AIAA, 2007.
[10] 刘睿, 白俊强, 邱亚松, 等.内吹式襟翼几何参数影响研究与优化设计[J].西北工业大学学报, 2020, 38(1):58-67. LIU R, BAI J Q, QIU Y S, et al.Effects of geometrical parameters of internal blown flap and its optimal design[J].Journal of Northwestern Polytechnical University, 2020, 38(1):58-67(in Chinese).
[11] 康辉.提高飞翼飞行器起降性能的腹部襟翼[J].国际航空, 2008(2):47. KANG H.Belly flap innovation for blended-wing body[J].International Aviation, 2008(2):47(in Chinese).
[12] DOUGHERTY D A.Wind tunnel test of a tailless aircraft with a belly-flap control surface used in combination with wing flaps[D].Long Beach:University of Southern California,2012:24-25.
[13] 石钧之, 王永恩, 张沛良, 等.二维翼型下表面增升辅助装置仿真及设计[J].飞机设计, 2019, 39(6):76-80. SHI J Z, WANG Y E, ZHANG P L, et al.Simulation and design of belly auxiliary device of lift-enhancement on the bottom of two-dimensional airfoil[J].Aircraft Design, 2019, 39(6):76-80(in Chinese).
[14] 米百刚, 詹浩, 朱军.二维干净构型、增升构型地面效应的数值模拟研究[J].应用力学学报, 2013, 30(6):822-827, 949. MI B G, ZHAN H, ZHU J.Numerical simulation on aerodynamic characteristic of clean and multi-element airfoils in ground effect[J].Chinese Journal of Applied Mechanics, 2013, 30(6):822-827, 949(in Chinese).
[15] 肖涛, 代钦.Gurney襟翼对机翼地面效应气动特性和流动结构的影响实验研究[J].空气动力学学报, 2013, 31(5):572-578. XIAO T, DAI Q.The experimental study of aerodynamics and flow structures of a wing with Gurney flaps in ground effect[J].Acta Aerodynamica Sinica, 2013, 31(5):572-578(in Chinese).
[16] 周铸, 黄江涛, 黄勇, 等.CFD技术在航空工程领域的应用、挑战与发展[J].航空学报, 2017, 38(3):020891. ZHOU Z, HUANG J T, HUANG Y, et al.CFD technology in aeronautic engineering field:Applications, challenges and development[J].Acta Aeronautica et Astronautica Sinica, 2017, 38(3):020891(in Chinese).
[17] 黄江涛, 张绎典, 高正红, 等.基于流场/声爆耦合伴随方程的超声速公务机声爆优化[J].航空学报, 2019, 40(5):122505. HUANG J T, ZHANG Y D, GAO Z H, et al.Sonic boom optimization of supersonic jet based on flow/sonic boom coupled adjoint equations[J].Acta Aeronautica et Astronautica Sinica, 2019, 40(5):122505(in Chinese).
[18] 桂业伟, 周志宏, 李颖晖, 等.关于飞机结冰的多重安全边界问题[J].航空学报, 2017, 38(2):520734. GUI Y W, ZHOU Z H, LI Y H, et al.Multiple safety boundaries protection on aircraft icing[J].Acta Aeronautica et Astronautica Sinica, 2017, 38(2):520734(in Chinese).
[19] 崔钊, 韩东, 李建波.翼型加装格尼襟翼的高亚声速气动特性研究[J].航空学报, 2013, 34(10):2277-2286. CUI Z, HAN D, LI J B.Study on aerodynamic characteristics of airfoil with gurney flaps under high subsonic flow[J].Acta Aeronautica et Astronautica Sinica, 2013, 34(10):2277-2286(in Chinese).
[20] 屈秋林, 刘沛清.地效飞行器地面巡航气动性能数值模拟及分析[J].航空学报, 2006, 27(1):16-22. QU Q L, LIU P Q.Numerical simulation and analysis of aerodynamics of WIG craft in cruise over ground[J].Acta Aeronautica et Astronautica Sinica, 2006, 27(1):16-22(in Chinese).
[21] 应成炯, 杨韡, 杨志刚.地面效应下的机翼失速数值模拟[J].飞行力学, 2010, 28(5):9-12, 15. YING C J, YANG W, YANG Z G.Numerical simulation on stall of wing in ground effect[J].Flight Dynamics, 2010, 28(5):9-12, 15(in Chinese).
[22] 秦绪国, 刘沛清, 屈秋林, 等.三维多段机翼地面效应数值模拟[J].航空学报, 2011, 32(2):257-264. QIN X G, LIU P Q, QU Q L, et al.Numerical simulation on 3D multi-element wings in ground effect[J].Acta Aeronautica et Astronautica Sinica, 2011, 32(2):257-264(in Chinese).
[23] 朱一西, 陆志良, 郭同庆, 等.飞机着陆过程中非定常地面效应数值模拟方法[J].航空计算技术, 2017, 47(4):103-106. ZHU Y X, LU Z L, GUO T Q, et al.Numerical simulation of landing aircraft in unsteady ground effect[J].Aeronautical Computing Technique, 2017, 47(4):103-106(in Chinese).
CJA