推进技术 ›› 1997, Vol. 18 ›› Issue (5): 50-52.

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再入飞行器化学非平衡流动的隐式向量算法研究

曾明,王正华,柳军,瞿章华,陈宏   

  1. 国防科技大学航天技术系!长沙;410073;国防科技大学航天技术系!长沙;410073;国防科技大学航天技术系!长沙;410073;国防科技大学航天技术系!长沙;410073;国防科技大学航天技术系!长沙;410073
  • 发布日期:2021-08-15
  • 基金资助:
    国家自然科学基金!19382001;“并行与分布处理国防科技重点实验室”资助

VECTORIZATION OF THE IMPLICIT SOLUTION FOR CHEMICAL NONEQUILBRIUM FLOW OVER REENTRY VEHICLE

  1. Dept. of Aerospace Technology, National Univ. of Defense Technology, Changsha, 410073;Dept. of Aerospace Technology, National Univ. of Defense Technology, Changsha, 410073;Dept. of Aerospace Technology, National Univ. of Defense Technology, Changsha, 410073;Dept. of Aerospace Technology, National Univ. of Defense Technology, Changsha, 410073;Dept. of Aerospace Technology, National Univ. of Defense Technology, Changsha, 410073
  • Published:2021-08-15

摘要: 在YH-2计算机上对再入飞行器化学非平衡流流场的NND隐式程序进行向量化计算,在对程序作了重构优化后,向量加速比达3.4。这是对化学非平衡流N-S方程隐式程序进行向量化计算的成功尝试,也为进一步实现程序的并行执行奠定了良好的基础。

关键词: 再入飞行器;非平衡流;向量运算;计算机技术

Abstract: Numerical simulation code of chemical nonequilibrium flow over reentry vehicle isvectorized in YH-2 supercomputer. Speedup ratio of vectorization reaches 3. 4 after reconstruction andoptimization of the scalarcode. This is a successful attempt at vectorizating Navier-Stokes equationsimplicit solution for chemical nonequilibrium flow, and it provides a good basis for parallel processingof the code.

Key words: Reentry vehiclc;Nonequilibrium flow;Vector operational;Computer technique