期刊文献+
任意字段
题名或关键词
题名
关键词
文摘
作者
第一作者
机构
刊名
分类号
参考文献
作者简介
基金资助
栏目信息

潜艇指挥室围壳顶部型线构型 被引量：6

Optimal design of the top form of submarine sail
下载PDF
导出
摘要 采用求解RANS方程的数值计算方法,运用计算流体力学数值计算手段,对不同的指挥室围壳顶部外型进行阻力、流场、压力分布数值模拟及数值优化分析,并验证了数值计算方法的可靠性。 The FLUENT software was used to solve the RANS equation numerically, in order to analyze the resistance, flow field and pressure distribution for different top form of submarine sail. The numerical optimization analysis is carried out also. The results can be used in the design of top form of submarine sail.
作者 杜波 黄建伟 陈源
机构地区 武汉第二船舶设计研究所
出处 《船海工程》 北大核心 2007年第2期107-110,共4页 Ship & Ocean Engineering
关键词 CFD 潜艇 围壳顶部型线 数值优化 CFD submarine top form of sail numerical optimization
分类号 U661.1 [交通运输工程—船舶及航道工程]
  • 相关文献

参考文献4

二级参考文献31

  • 1[1]Li Tiansen. Torpedo maneuverability[M]. (In Chinese) China National Defense Industry Press, 1999.
  • 2[2]Roddy Robert F. Investigation of the stability and control characteristics of several configurations of the DARPA SUBOFF model (DTRC model 5470) from captive-model experiments[R]. AD-A227 715,1990.
  • 3[3]Tang Denghai. Design of an axis-symmetric hull and its stern ring wing[R]. CSSRC Report No.02015 (In Chinese), 2002.
  • 4[4]Xia Xian, et al. Experimental study on the fluid dynamics of a body of revolution with stern wings, part 1: fluid-dynantic forces[R]. CSSRC Report No.03130 (In Chinese), 2002.
  • 5[5]Xia Xian, et al. Experimental study on the fluid dynamics of a body of revolution with stern wings, part 2: surface pressure distribution[R]. CSSRC Report (In Chinese), 2002.
  • 6[6]Hong Fangwen. Prediction of the flow around a body of revolution with stem wings with CFD[R]. CSSRC Report No. 03123 (In Chinese), 2002.
  • 7[7]Pan Ziying. Investigation of CFD application to prediction of the hydrodynamic forces on submersible vehicles at angles of attack[R]. CSSRC Report No. 03298 (In Chinese),2003.
  • 8[8]Tian Yukui. Wind tunnel test report of a torpedo-like body with a duct[R]. CSSRC Report No. 02254 (In Chinese), 2003.
  • 9[9]Parlett Lysle P. Aerodynamic Characteristic of a Small-Scale Shrouded Propeller at Angles of Attack from 0° to 90°[Z]. NACA TN3547, 1957.
  • 10[1]Chesnakas C J, Simpson R L. Detailed investigation of the three-dimensional separation about a 6:1 prolate spheroid[J].AIAA Journal, 1997,35(6).

共引文献108

同被引文献65

引证文献6

二级引证文献21

船海工程
2007年 第2期

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部