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Time accurate simulation of hypervelocity base flows on massively parallel computers.

机译:在大型并行计算机上对超高速基流进行时间精确的仿真。

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摘要

The efficient design of thermal protection systems (TPS) for vehicles entering planetary atmospheres requires a detailed knowledge of the flowfield which envelops the vehicle during a hypervelocity entry. The size, shape, and thermodynamic state of the base flow generated behind such a body determines the size of the after body and the required heat shielding. For many years experimental evidence has indicated that the base flow was unsteady, but there was not sufficient data to understand or characterize this unsteady behavior.;In order to simulate numerically the time dependent behavior of these flow fields, it would be necessary to compute a three dimensional flow field on a mesh with a level of resolution adequate to resolve the complex features observed in hypervelocity base flows. These types of computations are prohibitively expensive in terms of total CPU hours and actual turn around times.;The focus of the current research was to investigate the time dependent nature of hypervelocity base flows while developing computational techniques to allow time accurate simulations to be more routinely performed in the future.;The latter goal was addressed by exploiting the emerging power of massively parallel supercomputers. In the course of this research a parallel extension to the traditional Gauss-Seidel line relaxation algorithm was developed and tested. This algorithm is referred to as Block Implicit Gauss-Seidel line relaxation and achieves high performance on parallel computers by limiting global communication. In general, large simulations can be run 4 to 8 times faster than on the Cray C-90 supercomputer.;The former goal was addressed by applying the previously developed computational tools to the time accurate simulation of hypervelocity base flows. The resulting computations verified that the unsteady character of the base flow was indeed computable. In fact, the computed results were in agreement with experimental observations. Furthermore, the computations strongly suggested that a mechanism of unsteadiness was the amplification of oscillations in the wake shear layers. Hence, shear layer instability may drive the time dependent nature of these flows.
机译:用于进入行星大气的车辆的热保护系统(TPS)的有效设计需要对流场的详细了解,该流场会在超高速进入过程中包围车辆。在这种主体后面产生的基本流的大小,形状和热力学状态决定了后主体的大小和所需的隔热效果。多年来的实验证据表明,基本流是不稳定的,但是没有足够的数据来理解或表征这种不稳定的行为。为了对这些流场的时间相关行为进行数值模拟,有必要计算网格上的三维流场,其分辨率足以解决超高速基流中观察到的复杂特征。就总CPU时间和实际周转时间而言,这些类型的计算非常昂贵。;当前研究的重点是研究超高速基流的时间依赖性,同时开发计算技术以更常规地进行时间精确的模拟后一个目标是通过利用大规模并行超级计算机的新兴功能来解决的。在这项研究过程中,对传统的高斯-赛德尔线松弛算法进行了并行扩展,并进行了测试。该算法称为块隐式高斯-赛德尔线松弛,通过限制全局通信在并行计算机上实现高性能。通常,大型仿真的运行速度比Cray C-90超级计算机快4至8倍。以前的目标是通过将先前开发的计算工具应用于超高速基流的时间精确仿真来解决的。所得的计算结果证明了基本流的不稳定特性确实是可计算的。实际上,计算结果与实验观察结果一致。此外,计算结果强烈表明,不稳定的机制是尾流剪切层中振荡的放大。因此,剪切层的不稳定性可能会驱动这些流的时间依赖性。

著录项

  • 作者

    Anagnost, Andrew John.;

  • 作者单位

    Stanford University.;

  • 授予单位 Stanford University.;
  • 学科 Aerospace engineering.;Mechanical engineering.
  • 学位 Ph.D.
  • 年度 1994
  • 页码 142 p.
  • 总页数 142
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:49:59

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