[1] Vicente N M, Piechocki J, Cuerva A, et al.Experimental research on a vertically falling rotating wing decelerator model[C]//19th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.Reston: AIAA, 2007.
[2] Vicente N M, Angel S A, Alvaro C. Experimental investigation of an autorotating-wing aerodynamic decelerator system[C]//18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. Reston: AIAA, 2005.
[3] Crimi P. Finite element analysis of a samara-wing decelerator[J]. Journal of Aircraft, 1996, 33(4): 793-802.
[4] Borgstrom D, Paulsson L, Karlsen L. Aerodynamics of a rotating body descending from the separation position of an artillery munition shell, AIAA-1991-0870[R]. Reston: AIAA, 1991.
[5] Shu J R. Study on the large angle of attack scanning characteristic of asymmetric terminal sensing submunition and its application[D]. Nanjing: Nanjing University of Science and Technology, 2004 (in Chinese). 舒敬荣. 非对称末敏子弹大攻角扫描特性研究及应用[D]. 南京: 南京理工大学, 2004.
[6] Shu J R, Zhang B C, Han Z P, et al. A study on the scanning motion of single-fin target sensitivity projectile[J]. Acta Armamentarii, 2004, 25(4): 415-420 (in Chinese). 舒敬荣, 张邦楚, 韩子鹏, 等. 单翼末敏弹扫描运动研究[J]. 兵工学报, 2004, 25(4): 415-420.
[7] Shu J R, Liu C Y, Han Z P, et al. Study on scanning motion of flexible single-fin terminal sensing ammunition[J]. Journal of Ballistics, 2004, 16(1): 36-42 (in Chinese). 舒敬荣, 刘昌源, 韩子鹏, 等. 柔性单翼末敏弹扫描运动研究[J]. 弹道学报, 2004, 16(1): 36-42.
[8] Gu J P, Han Z P. Comparison and analyses of single-fin TSA's and parachute TSA's scanning[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011, 31(1): 123-124 (in Chinese). 顾建平, 韩子鹏. 单翼与有伞末敏子弹的扫描比较及分析[J]. 弹箭与制导学报, 2011, 31(1): 123-124.
[9] Gu J P, Han Z P. Application of quaternionin in single-fin terminal sensing ammunition scanning simulation[J]. Journal of Ballistics, 2010, 22(4): 15-18 (in Chinese). 顾建平, 韩子鹏. 四元数在单翼末敏弹扫描仿真中的应用[J]. 弹道学报, 2010, 22(4): 15-18.
[10] Wang A Z. The study on stable scanning characteristics of non-parachute terminal sensitive projectile[D]. Nanjing: Nanjing University of Science and Technology, 2008 (in Chinese). 王爱中. 无伞末敏弹稳态扫描特性研究[D]. 南京: 南京理工大学, 2008.
[11] Zhou S Y. Research on the model and calculation methods for the stable scanning of a terminal-sensitive projectile without parachute[D]. Nanjing: Nanjing University of Science and Technology, 2010 (in Chinese). 周思渊. 无伞末敏弹稳态扫描运动模型与计算方法研究[D]. 南京: 南京理工大学, 2010.
[12] Wang L X. Research on the design methods for the stable scanning of a terminal-sensitive ammunition without parachute[D]. Nanjing: Nanjing University of Science and Technology, 2013 (in Chinese). 王刘星. 双翼无伞末敏弹扫描运动设计方法研究[D]. 南京: 南京理工大学, 2013.
[13] Shi J G, Han Z P, Shu J R, et al. Stable scanning model for non-parachute terminal sensitive projectile with two fins[J]. Journal of Ballistics, 2010, 22(2): 24-27 (in Chinese). 史金光, 韩子鹏, 舒敬荣, 等. 双翼型无伞末敏弹稳态扫描运动数学模型[J]. 弹道学报, 2010, 22(2): 24-27.
[14] Shu J R, Jiang S P, Li M J, et al. Forces and moments analysis for double-win terminal sensing ammunition without parachute at the stage of stable-scanning[J]. Journal of Ballistics, 2010, 22(2): 48-51 (in Chinese). 舒敬荣, 蒋胜平, 李明军, 等. 无伞双翼末敏弹稳态扫描段受力分析[J]. 弹道学报, 2010, 22(2): 48-51.
[15] Hu Z P, Liu R Z, Guo R. Effect of two typical wing shapes on aerodynamic characteristics of non-parachute terminal sensitive projectile[J]. Journal of Nanjing University of Science and Technology, 2012, 36(5): 740-744 (in Chinese). 胡志鹏, 刘荣忠, 郭锐. 两种典型尾翼形状对无伞末敏弹气动特性的影响[J]. 南京理工大学学报, 2012, 36(5): 740-744.
[16] Hu Z P, Liu R Z, Guo R. The dual-wings terminal sensitive projectile bending angle effect on the aerodynamic characteristics[J]. Acta Aerodynamic Sinica, 2014, 32(1): 62-68 (in Chinese). 胡志鹏, 刘荣忠, 郭锐. 无伞末敏弹双S形尾翼弯折角对气动特性影响研究[J]. 空气动力学学报, 2014, 32(1): 62-68.
[17] Hu Z P, Liu R Z, Guo R. Aerodynamic characteristics of two wings terminal sensitive projectile based on FLUENT[J]. Flight Dynamics, 2013, 31(1): 53-56 (in Chinese). 胡志鹏, 刘荣忠, 郭锐. 基于FLUENT的双翼末敏弹气动特性研究[J]. 飞行力学, 2013, 31(1): 53-56.
[18] Lyu S T, Liu R Z, Guo R, et al. Optimum design on aerodynamic configuration of terminal sensitive projectile with S-C style wings[J]. Journal of Ballistics, 2014, 26(2): 6-11 (in Chinese). 吕胜涛, 刘荣忠, 郭锐, 等. S-C型双翼末敏弹尾翼结构方案设计[J]. 弹道学报, 2014, 26(2): 6-11.
[19] Lyu S T, Liu R Z, Guo R, et al. Optimum design on aerodynamic shape of the S-S style non-parachute terminal sensitive projectile[J]. Acta Armamentarii, 2013, 34(9): 1150-1154 (in Chinese). 吕胜涛, 刘荣忠, 郭锐, 等. S-S双翼末敏弹气动外形优化设计[J]. 兵工学报, 2013, 34(9): 1150-1154.
[20] Zhou Z C, Zhao R X, Han Z P, et al. The aerodynamic shape design and aerodynamic characteristics analysis of terminal sensing submunition[J]. Acta Aerodynamica Sinic, 2012, 31(1): 15-21 (in Chinese). 周志超, 赵润祥, 韩子鹏, 等. 末敏子弹气动外形设计与气动特性分析[J]. 空气动力学学报, 2012, 31(1): 15-21.
[21] Zhou Z C, Zhao R X, Han Z P, et al. Wind tunnel experimental investigation on aerodynamic characteristics of non-parachute terminal sensitive ammunition[J]. Journal of Experimental Mechanics, 2012, 27(2): 183-188 (in Chinese). 周志超, 赵润祥, 韩子鹏, 等. 无伞末敏弹气动特性风洞实验研究[J]. 实验力学, 2012, 27(2): 183-188.
[22] Han Z P. Exterior ballistics of projectile and rochet[M]. Beijing: Publishing House of Beijing Institute of Technology, 2008: 189-193, 296-302 (in Chinese). 韩子鹏. 弹箭外弹道学[M]. 北京: 北京理工大学出版社, 2008: 189-193, 296-302.
[23] Li C M, Liu Y X. Influence of unsymmetrical equatorial damp moment on long range rockets trajectory[J]. Journal of Ballistics, 2009, 21(2): 36-39 (in Chinese). 李臣明, 刘怡昕. 非对称赤道阻尼力矩对远程火箭弹道的影响[J]. 弹道学报, 2009, 21(2): 36-39. |