| [1] Wu J F, Luo X F, Fan Z L. Flow control method to improve cavity flow and store separation characteristics[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(10):1840-1845.(in Chinese) 吴继飞, 罗新福, 范召林.内埋式弹舱流场特性及武器分离特性改进措施[J].航空学报, 2009, 30(10): 1840-1845.[2] Feng Q, Cui X C. Study on integrated flow control for weapons bay of flying wing configuration aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(5): 781-787.(in Chinese) 冯强, 崔晓春.飞翼布局武器舱综合流动控制技术研究[J].航空学报, 2012, 33(5): 781-787.[3] Yang D G, Fan Z L, Li J Q, et al. Studies on flow characteristics of cavity by numerical simulation and wind tunnel test[J]. Acta Aerodynamica Sinica, 2009, 27(3): 378-383.(in Chinese) 杨党国, 范召林, 李建强, 等.弹舱流动特性数值模拟及风洞试验研究[J].空气动力学学报, 2009, 27(3): 378-383.[4] Li J, Li T, Zhang Q F. The mechanism and control of a open cavity flow[J]. Journal of Experiments in Fluid Mechanics, 2008, 22(1): 80-83.(in Chinese) 黎军, 李天, 张群峰.开式流动舱体的流动机理与控制[J]. 实验流体力学, 2008, 22(1): 80-83.[5] Wu J F, Tao Y, Fan Z L, et al. Analysis of the effect of the modification at the trailing edge on cavity flow characteristics[J]. Acta Aerodynamica Sinica, 2010, 28(2):197-202.(in Chinese) 吴继飞, 陶洋, 范召林, 等.后缘修型对空腔流场特性影响分析[J].空气动力学学报, 2010, 28(2): 197-202.[6] Luo X F, Fan Z L. The firs modern experimental aerodynamics of corpus//Experimental Investigation on Internal Weapon bay Flow Characteristics and Its Flow Control. Beijing: Atomic Press, 2007.[7] Zhang N, Alvi F S, Alkislar M B, et al.Aeroacoustic properties of supersonic cavity flow and their control, AIAA-2003-3101. Reston: AIAA, 2003.[8] Raman G, Kibens V. Active flow control using integrated powered resonance tube actuators, AIAA-2001-3024. Reston: AIAA, 2001.[9] Grove J E, Birkbeck R M, Kreher J M. Acoustic and separation characteristics with bay leading edge blowing, AIAA-2000-1904. Reston: AIAA, 2000.[10] Smith B R, Welterlen T J, Maines B H, et al. Weapons bay acoustic suppression from rod spoilers, AIAA-2002-0662. Reston: AIAA, 2002.[11] Cattafesta L, Williams D R, Rowley C W, et al. Review of active control of flow induced cavity resonance, AIAA-2003-3567. Reston: AIAA, 2003.[12] Liu Y. Fluid dynamica analysis on missile launching and separating from weapon bay. Nanjing: Nanjing University of Aeronautics and Astronautics, 2010.(in Chinese) 刘瑜. 内埋式弹舱武器发射分离过程研究.南京: 南京航空航天大学, 2010.[13] Zhang B B. Numerical simulation and control of cavity flow. Nanjing: Nanjing University of Aeronautics and Astronautics, 2011.(in Chinese) 张宝兵. 空腔流动的机理模拟与控制. 南京: 南京航空航天大学, 2011.[14] Wang W. Aerodynamic studies and simulation of missiles internal. Harbin: Harbin Engineering University, 2011.(in Chinese) 王巍. 导弹内埋气动特性研究与仿真. 哈尔滨: 哈尔滨工业大学, 2011.[15] Huang X H, Luo X F, Yu Z S. Design & development of a new captive trajectory simulation system in FL-24 wind tunnel[J]. Acta Aerodynamica Sinica, 2008, 26(2): 145-149.(in Chinese) 黄叙辉, 罗新福, 于志松.FL-24风洞新型捕获轨迹系统设计与发展[J].空气动力学学报, 2008, 26(2): 145-149.[16] Yu Z S, Wang F X, Luo X F. Investigation of two special CTS test techniques[J].Experiments and Measurements in Fluid Mechanics, 2004, 18(4): 49-53.(in Chinese) 于志松, 王发祥, 罗新福. 两种特殊CTS试验技术的研究[J]. 流体力学试验与测量, 2004, 18(4): 49-53. |
CJA
