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首页> 外文期刊>Journal of Spacecraft and Rockets >Time-Accurate Coupling of Three-Degree-of-Freedom Parachute System with Navier-Stokes Equations
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Time-Accurate Coupling of Three-Degree-of-Freedom Parachute System with Navier-Stokes Equations

机译:具有Navier-Stokes方程的三自由度降落伞系统的时间精确耦合

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摘要

A parachute with payload is modeled as a three-degree-of-freedom system suitable for time-accurate coupling with the Navier-Stokes flow equations. The coupled equations of motion are formulated following an instantaneous Lagrangian-Eulerian approach, and solved using Newmark's time-integration method. Flow solutions are computed by solving the Reynolds-averaged Navier-Stokes equations with structured overset grids. A sensitivity analysis is used to check the adequacy of grid and time-step requirements. The time-accurate coupling procedure is validated by comparing the results with a frequency-domain approach. The results are demonstrated for a real parachute system, including a comparison with the results based on the linear theory. Possible instabilities, such as divergence of inclination angle and flutter associated with fluctuating drag force, are predicted. The present work advances the fidelity of analysis procedures beyond those in current use based on loose coupling with the Navier-Stokes equations.
机译:带有有效载荷的降落伞被建模为三自由度系统,适合与Navier-Stokes流量方程式进行时间精确的耦合。耦合的运动方程式是根据瞬时拉格朗日-欧拉方法制定的,并使用Newmark的时间积分方法求解。流量解是通过对具有结构化过顶网格的雷诺平均Navier-Stokes方程进行求解来计算的。敏感性分析用于检查网格和时间步长要求的适当性。通过将结果与频域方法进行比较,可以验证时间精确的耦合过程。实际降落伞系统的结果得到了证明,包括与基于线性理论的结果的比较。可以预测可能的不稳定性,例如倾斜角的发散和与波动力相关的颤动。基于与Navier-Stokes方程的松耦合,当前的工作超出了当前使用的分析程序的保真度。

著录项

  • 来源
    《Journal of Spacecraft and Rockets 》 |2017年第6期| 1278-1283| 共6页
  • 作者

    Guruswamy G. P.;

  • 作者单位

    NASA, Ames Res Ctr, Computat Phys Branch, Moffett Field, CA 94035 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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