共被期刊论文引用了4次
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| 1 | 双组尾翼弹气动特性计算与分析显示文摘本文根据双组尾翼弹的外形特点,选用了代数网格生成方法,通过求解N S方程,对其气动特性进行了数值计算,并对其计算结果进行了分析。由计算结果可知,此种弹的双尾翼可以为其提供一定的转速和升力,提高其静稳定性。并且此种弹已经用于型号设计。 | 武频 赵润祥 郭锡福 | 2002 | 空气动力学学报2002，20，4： | 5 |
| 2 | 弹丸速度与弹道倾角之间的近似公式显示文摘运用近似公式定量分析过弹道顶点后一段时间内弹丸速度和弹道倾角之间的规律 ,解决了以往只能定性分析而不能定量分析的难题 . | 安长星 郝博 | 2003 | 沈阳工业学院学报2003，22，2： | 1 |
| 3 | Aerodynamic Characteristics of Projectile with Exotic Wraparound Wings Configuration显示文摘A projectile with exotic wraparound wings( WAW) configuration is designed to improve the finstabilized projectile shooting quality. Two fin-stabilized projectiles with the same body with and without exotic WAW configuration are simulated numerically by applying the Roe scheme. The shear-stress transport turbulence models and the lower-upper symmetric Gauss-Seidel implicit method are used to solve 3D Reynoldsaveraged Navier—Stokes equations. The differences in aerodynamic coefficients and aerodynamic characteristics of the projectiles when the Mach number varies from 0. 35 to 0. 95 are obtained,and the cause of these differences is analyzed. The calculation results indicate that the lift-to-drag ratio of the projectile significantly increases,the rolling moment decreases,and the position of the pressure center of the projectile shows relatively small changes when the exotic WAW configuration is used. Therefore,this projectile can obviously reduce rolling effect,enlarge range and improve flying stability. | Fu Zhang Wen-Jun Ruan Hao Wang Chen-Guang Zhu Meng-Hua Zhang | 2014 | Journal of Harbin Institute of Technology(New Series)2014，21，3： | 0 |
| 4 | 基于视频的弹丸终点参数获取研究显示文摘针对目前弹丸动爆实验组织难,系统复杂等问题,论文提出了一种基于视频图像计算弹丸终点参数的新方法,简化了动爆实验所需的复杂测量系统平台,通过视频图像中弹丸位置姿态的提取计算弹丸终点参数。论文采用了改进的减背景法进行目标定位与跟踪,根据弹丸边界确定弹丸姿态,再由投影变换和立体视觉原理求得目标实际位置和姿态,并运用VC2010和OpenCV2.2软件平台设计了仿真系统。系统仿真结果表明论文方法实用可行,运算速度快,精度较高。 | 曹丽静 刘玉文 | 2015 | 舰船电子工程2015，35，4： | 0 |
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