[1] RASMUSSEN C C, CANFIELD R A, BLAIR M. Joined-wing sensor-craft configuration design[J]. Journal of Aircraft, 2006, 43(5):1470-1478.
[2] MARTINEZ J, FLICK P, PERDZOCK J, et al. An overview of sensorcraft capabilities and key enabling technologies:AIAA-2008-7185[R]. Reston, VA:AIAA, 2008.
[3] WOLKOVITCH J. The joined wing:An overview[J]. Journal of Aircraft, 1986, 23(3):161-178.
[4] KROO I, SMITH S, GALLMAN J. Aerodynamic and structural studies of joined-wing aircraft[J]. Journal of Aircraft, 1991, 28(1):74-81.
[5] LIVNE E. Aeroelasticity of joined-wing airplane configurations:Past work and future challenges-A survey:AIAA-2001-1370[R]. Reston, VA:AIAA, 2001.
[6] CRAFT R L. Drag estimates for the joined-wing sensor craft[D]. Dayton, OH:Wright-Patterson Air Force Base, 2005.
[7] LEDOUX S, VASSBERG J, FATTA G, et al. Aerodynamic cruise design of a joined wing sensorcraft:AIAA-2008-7190[R].Reston, VA:AIAA, 2008.
[8] 曹晨. 机载相控阵PD雷达性能分析中的重要问题[J]. 现代雷达,2008, 30(6):14-16. CAO C.Problems in airborne phased-array PD radar performance analysis[J]. Modern Radar, 2008, 30(6):14-16(in Chinese).
[9] 张晓波, 曹晨. 机载预警雷达最优探测波长研究[J]. 中国电子科学研究院学报, 2011, 6(3):263-266. ZHANG X B, CAO C. A study on airborne early warning radar optimal detection wavelength[J]. Journal of CAEIT, 2011, 6(3):263-266(in Chinese).
[10] 李相如, 曹晨. 机载预警雷达搜索参数研究[J]. 中国电子科学研究院学报, 2015, 10(4):406-410. LI X R, CAO C.The research on airborne early warning radar search parameters[J]. Journal of CAEIT, 2015, 10(4):406-410(in Chinese).
[11] 王科雷, 周洲, 许晓平, 等. 超临界翼型低雷诺数流动分析及优化设计[J]. 航空学报, 2015,36(10):3275-3283. WANG K L, ZHOU Z, XU X P, et al. Flow characteristics analysis and optimization design of supercritical airfoil at low Reynolds number[J]. Acta Aeronautica et Astronautica Sinica, 2015,36(10):3275-3283(in Chinese).
[12] 王科雷, 周洲, 甘文彪, 等. 太阳能无人机低雷诺数翼型气动特性研究[J]. 西北工业大学学报, 2014, 32(2):163-168. WANG K L, ZHOU Z,GAN W B, et al. Studying aerodynamic performances of the low-Reynolds-number airfoil of solar energy UAV[J]. Journal of Northwestern Polytechnical University, 2014, 32(2):163-168(in Chinese).
[13] GREER D, HAMORY P, EDWARDS C, et al. Design and predictions for high-altitude (low Reynolds number) aerodynamic flight experiment[J]. Journal of Aircraft, 2000, 37(4):684-689.
[14] 左林玄, 王晋军. 低雷诺数翼型的优化设计[J]. 兵工学报, 2009,30(8):1073-1077. ZUO L X, WANG J J. Airfoil design optimization at low Reynolds number[J]. Acta Armamentarii, 2009,30(8):1073-1077(in Chinese).
[15] WANG Z Y, ZHU X P, ZHOU Z, et al. A numerical research on aerodynamic interference of diamond-wing sensor-craft[C]//7th Asia-Pacific International Symposium on Aerospace Technology, 2015:545-552.
[16] 孙俊磊,王和平,周洲,等.菱形连翼布局俯仰力矩非线性特性数值分析[J]. 北京航空航天大学学报,2017,43(8):1567-1576. SUN J L, WANG H P, ZHOU Z, et al. Numerical analysis of pitching moment non-linear characteristics of diamond joined-wing configuration[J]. Journal of Beijing University of Aeronautics and Astronautics,2017,43(8):1567-1576(in Chinese).
[17] 杨青真,张仲寅.超临界层流机翼边界层及气动特性分析[J].航空学报,2004,25(5):438-442. YANG Q Z, ZHANG Z Y. Analysis of the boundary layer and aerodynamic characteristics of a supercritical laminar wing[J]. Acta Aeronautica et Astronautica Sinica, 2004, 25(5):438-442(in Chinese).
[18] SKOLNIK M I.雷达手册[M]. 北京:电子工业出版社,2003:556-558. SKOLNIK M I. Radar handbook[M]. Beijing:Publishing House of Electronics Industry, 2003:556-558(in Chinese).
[19] COOK P H, LOCK R C. Aerofoil RAE2822-pressure distributions and boundary layer and wake measurements:AGARD-AR-138[R]. Brussels:AGARD, 1979.
[20] HICKS R M, HENNE P A. Wing design by numerical optimization[J]. Journal of Aircraft, 1978, 15(7):407-412.
[21] 王建军, 高正红. HicksHenne翼型参数化方法分析及改进[J]. 航空计算技术, 2010, 40(4):46-49. WANG J J,GAO Z H. Analysis and improvement of HicksHenne airfoil parameterization method[J]. Aeronautical Computing Technique, 2010, 40(4):46-49(in Chinese).
[22] 王小平,曹立明.遗传算法:理论、应用与软件实现[M]. 西安:西安交通大学出版社,2002:11-17. WANG X P,CAO L M. Genetic algorithm:Theory, application and realization[M]. Xi'an:Xi'an Jiaotong University Press,2002:11-17(in Chinese).
[23] 赖宇阳. Isight参数优化理论与实例详解[M].北京:北京航空航天大学出版社,2012:117-127. LAI Y Y. Optimization theory and detailed examples of Isight[M]. Beijing:Beihang University Press,2012:117-127(in Chinese).
[24] LEVIN O, WEI S. Optimization of a flexible low Reynolds number airfoil:AIAA-2001-0125[R]. Reston,VA:AIAA, 2001. |