...
首页> 外文期刊>Defence science journal >Asymmetrical Vortex over Slender Body A Computational Approach
【24h】

Asymmetrical Vortex over Slender Body A Computational Approach

机译:在细长的身体上的不对称涡旋计算方法

获取原文
   

获取外文期刊封面封底 >>

       

摘要

Computational investigations were carried out on an ogive-cylinder configuration having a slenderness ratio of 7.5. The geometry of the nose tip was generated based on the physical geometry of the nose tip observed under a scanning electron microscope. Time-dependent simulations were performed on the slender body at a diameter Reynolds number of 3.0×104 . Results indicated that the onset of vortex asymmetry was mainly due to the microtip imperfection existing at the tip. It was also observed that the variation in the roll angle of the model affected the flow physics largely which has been experimentally observed by several researchers in the past. The computed results were in better agreement with the referenced experimental data.
机译:在具有细长比为7.5的初始缸体结构上进行计算研究。 基于在扫描电子显微镜下观察到的鼻尖的物理几何形状产生鼻尖的几何形状。 在直径雷诺数为3.0×104的直径雷诺数上进行时间依赖性模拟。 结果表明,涡流不对称的发作主要是由于尖端存在的微透明缺陷。 还观察到,模型的卷角的变化主要受到过去几个研究人员通过实验观察的流理物理。 计算结果与参考的实验数据更好。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号