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LAMINAR FLOW OVER A SPINNING PROJECTILE AT AN ANGLE OF ATTACK.

机译:在攻击角度旋转的弹丸上的层流。

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摘要

The study of forces and moments on a spinning pointed body at an angle of attack is extremely important in ballistics. Previous work has been mostly experimental. This is because the governing Navier-Stokes equations are nonlinear and fully three dimensional, making analysis impossible and direct numerical solutions impractical.; The most promising theoretical technique is the unsteady cross flow analogy. Considering the axial direction as timelike, the pressure and the flow field can be obtained from the impulsive starting of a two-dimensional cylinder. Although the analogy is heuristic, the results do correlate well with experimental data on slender bodies for subsonic through supersonic free stream speeds.; In this study we investigate the impulsive starting of expanding, rotating cylinders. The results are used to calculate the force and moment coefficients for projectiles by means of the unsteady cross-flow analogy. We solve the unsteady Navier-Stokes equations using matched asymptotic inner-outer perturbation method and comparing these results with the solution obtained using numerical methods. Excellent agreement between the two methods has been established in the region where both solutions are valid.; The results obtained are consistent with existing experimental work. For example, a pair of secondary recirculating zones has been predicted, in addition to the well-known primary pair for high Reynolds numbers. The numerical scheme used showed stability and robustness in the integration of the full Navier-Stokes equations.
机译:在弹道学中,研究旋转的尖形物体以攻角的作用力和力矩非常重要。以前的工作主要是实验性的。这是因为控制的Navier-Stokes方程是非线性的并且是完全三维的,这使得分析变得不可能,直接的数值解也不切实际。最有前途的理论技术是非稳态横流类比。将轴向视为时间,可以从二维圆柱的脉冲启动中获得压力和流场。尽管类比是启发式的,但结果与超音速至超音速自由流速度下的亚音速细长体的实验数据确实相关。在这项研究中,我们研究了膨胀旋转气缸的脉冲启动。通过非稳态横流类比,将结果用于计算弹丸的力和力矩系数。我们使用匹配的渐近内外扰动方法求解非定常的Navier-Stokes方程,并将这些结果与使用数值方法获得的解进行比较。两种方法都在有效的地区建立了极好的协议。获得的结果与现有的实验工作一致。例如,除了众所周知的用于高雷诺数的初级对之外,还预测了一对次级再循环区。所使用的数值方案在完整的Navier-Stokes方程的积分中显示出稳定性和鲁棒性。

著录项

  • 作者

    YOUSSEF, FOUAD AHMED.;

  • 作者单位

    Michigan State University.;

  • 授予单位 Michigan State University.;
  • 学科 Engineering Aerospace.
  • 学位 M.Sc.
  • 年度 1987
  • 页码 119 p.
  • 总页数 119
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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