Citation: | Yan Shiwei, Jin Wenchao, Tan Dali, Tian Yun. Aerodynamic design and numerical analysis of jet cooling blast deflector[J]. Chinese Journal of Ship Research, 2019, 14(2): 99-106. DOI: 10.19693/j.issn.1673-3185.01146 |
[1] |
何庆林, 卢晶, 杨大鹏.舰载飞机发动机尾流场数值模拟[J].中国舰船研究, 2013, 8(5):13-18, 51. doi: 10.3969/j.issn.1673-3185.2013.05.003
He Q L, Lu J, Yang D P. Numerical simulation of the flowfield of carrier-based aircraft exhaust jet[J]. Chinese Journal of Ship Research, 2013, 8(5):13-18, 51(in Chinese). doi: 10.3969/j.issn.1673-3185.2013.05.003
|
[2] |
王超.舰载飞机发动机射流对甲板周围环境的影响[D].哈尔滨: 哈尔滨工程大学, 2008. http://cdmd.cnki.com.cn/Article/CDMD-10217-2009060355.htm
Wang C. The influence of aircraft engine's jet flow around ship deck[D]. Harbin: Harbin Engineering University, 2008(in Chinese). http://cdmd.cnki.com.cn/Article/CDMD-10217-2009060355.htm
|
[3] |
黄胜, 王超, 胡建.舰载飞机发动机喷流速度场研究[J].哈尔滨工程大学学报, 2009, 30(4):353-356. doi: 10.3969/j.issn.1006-7043.2009.04.002
Haung S, Wang C, Hu J. Research on velocity field of carrier-based aircraft engine's jet flow[J]. Journal of Harbin Engineering University, 2009, 30(4):353-356(in Chinese). doi: 10.3969/j.issn.1006-7043.2009.04.002
|
[4] |
徐凯.航母舰载机与偏流板的适配性研究[D].哈尔滨: 哈尔滨工程大学, 2011. http://cdmd.cnki.com.cn/Article/CDMD-10217-1012265527.htm
Xu K. Research of adaption between aircraft and jet blast deflector[D]. Harbin: Harbin Engineering University, 2011(in Chinese). http://cdmd.cnki.com.cn/Article/CDMD-10217-1012265527.htm
|
[5] |
吴始栋.航母偏流板的开发与研究[J].中外船舶科技, 2008(4):9-11. http://cdmd.cnki.com.cn/Article/CDMD-10217-1011021118.htm
|
[6] |
Wadley H N G, Queheillalt D T, Haj-Hariri H, et al. Method and apparatus for jet blast deflection: US, 20030164425A1[P]. 2007-06-12.
|
[7] |
Tangen S. Investigating separated shear layers for passive jet blast deflector cooling[C]//44th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada: AIAA, 2006.
|
[8] |
Fischer E C, Sowell D A, Wehrle J, et al. Cooled jet blast deflectors for aircraft carrier flight decks: US, 6575113B1[P]. 2003-06-10.
|
[9] |
Campion G. Blast deflector: US, 6802477B2[P]. 2004-10-12.
|
[10] |
李昶, 邱旭, 任明其.新型折流板装置发展综述及其拓扑优化研究[J].船舶工程, 2015, 37(1):15-19. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=cbgc201501004
Li C, Qiu X, Ren M Q. Development of new blast deflector and research of its topology optimization[J]. Ship Engineering, 2015, 37(1):15-19(in Chinese). http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=cbgc201501004
|
[11] |
王军旗, 李素循, 倪招勇, 等.数值模拟侧向超声速单喷流干扰流场特性[J].宇航学报, 2007, 28(3):598-602. doi: 10.3321/j.issn:1000-1328.2007.03.018
Wang J Q, Li S X, Ni Z Y, et al. Numerical simulation of characteristics of supersonic jet interaction flowfields[J]. Journal of Astronautics, 2007, 28(3):598-602(in Chinese). doi: 10.3321/j.issn:1000-1328.2007.03.018
|
[12] |
赵飞, 张延玲, 朱荣, 等.超音速射流流场中湍流模型[J].北京科技大学学报, 2014, 36(3):366-372. http://d.old.wanfangdata.com.cn/Periodical/bjkjdxxb201403014
Zhao F, Zhang Y L, Zhu R, et al. Turbulence model in supersonic jet flowfield[J]. Journal of University of Science and Technology Beijing, 2014, 36(3):366-372(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/bjkjdxxb201403014
|
[13] |
赵留平.舰载机发动机喷管高温高压流动特性仿真分析[J].舰船科学技术, 2016, 38(1):145-149. doi: 10.3404/j.issn.1672-7649.2016.1.031
Zhao L P. Numerical simulation for high temperature and high pressure flowfield of aircraft engine jet impingement[J]. Ship Science and Technology, 2016, 38(1):145-149(in Chinese). doi: 10.3404/j.issn.1672-7649.2016.1.031
|
[14] |
王松涛, 冯国泰, 王仲奇, 等.尾喷管内部及其射流流场的数值模拟[J].推进技术, 2000, 21(3):53-55. doi: 10.3321/j.issn:1001-4055.2000.03.016
Wang S T, Feng G T, Wang Z Q, et al. Numerical simulation of performance and jet flowfield of the nozzle[J]. Journal of Propulsion Technology, 2000, 21(3):53-55(in Chinese). doi: 10.3321/j.issn:1001-4055.2000.03.016
|
[15] |
赵一鹗, 余少志.复杂几何形状喷管内外三维流场的数值模拟[J].推进技术, 2000, 21(3):30-33. doi: 10.3321/j.issn:1001-4055.2000.03.009
Zhao Y E, Yu S Z. Numerical simulation on internal and external flowfields of nozzle with complex geometry[J]. Journal of Propulsion Technology, 2000, 21(3):30-33(in Chinese). doi: 10.3321/j.issn:1001-4055.2000.03.009
|
[16] |
Gerolymos G A, Vallet I, BöLcs P O, et al. Computation of unsteady three-dimensional transonic nozzle flows using k-ε turbulence closure[J]. AIAA Journal, 1996, 34(7):1331-1340. doi: 10.2514/3.13237
|
[17] |
Hoffmann K A, Suzen Y B, Papadakis M. Numerical computation of high speed exhaust flows: AIAA 95-0758[R]. Reno, NV, U.S.A: AIAA, 1995.
|
[18] |
乔渭阳, 蔡元虎, 齐少军, 等.次流喷射控制推力矢量喷管的流场数值模拟[J].推进技术, 2000, 21(6):18-20, 35. doi: 10.3321/j.issn:1001-4055.2000.06.005
Qiao W Y, Cai Y H, Qi S J, et al. Flowfield numerical modeling of the thrust vector control nozzle based on secondary flow injection[J]. Journal of Propulsion Technology, 2000, 21(6):18-20, 35(in Chinese). doi: 10.3321/j.issn:1001-4055.2000.06.005
|
[19] |
黄胜, 王超.基于的偏流导流板的初步设计[C]//黑龙江省造船工程学会2007年学会年会文集.[S.l.: s.n.], 2007.
|
[20] |
黄爱华, 段红春.某大型运输机发动机尾喷口射流参数研究[J].中国工程机械学报, 2016, 14(3):277-280. doi: 10.3969/j.issn.1672-5581.2016.03.018
Huang A H, Duan H C. Parametric study on engine nozzle jet for specific large aerotransport[J]. Chinese Journal of Construction Machinery, 2016, 14(3):277-280(in Chinese). doi: 10.3969/j.issn.1672-5581.2016.03.018
|
[21] |
郭涛.偏流板性能的分析与计算[D].哈尔滨: 哈尔滨工程大学, 2010. http://cdmd.cnki.com.cn/Article/CDMD-10217-1011021118.htm
Guo T. Performance analysis and calculation of drift plate[D]. Harbin: Harbin Engineering University, 2010(in Chinese). http://cdmd.cnki.com.cn/Article/CDMD-10217-1011021118.htm
|