Volume 30 Issue 10
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ZHU Zhi-bin, YUAN Xiang-jiang, CHEN Lin. Finite volume compact algorithm suited to computation of supersonic flow field[J]. Journal of Aerospace Power, 2015, 30(10): 2481-2487. doi: 10.13224/j.cnki.jasp.2015.10.022
Citation: ZHU Zhi-bin, YUAN Xiang-jiang, CHEN Lin. Finite volume compact algorithm suited to computation of supersonic flow field[J]. Journal of Aerospace Power, 2015, 30(10): 2481-2487. doi: 10.13224/j.cnki.jasp.2015.10.022

Finite volume compact algorithm suited to computation of supersonic flow field

doi: 10.13224/j.cnki.jasp.2015.10.022
  • Received Date: 2014-03-26
  • Publish Date: 2015-10-28
  • In order to combine the advantages, a compact scheme based on finite volume method was developed. A characteristic limiter was used to prevent non-physical oscillations across discontinuity, so the scheme was suited to simulate supersonic flows in aerospace flight. The performance of the scheme was assessed by computing several typical problems. Numerical results reveal that the present scheme can capture discontinuities with few oscillations and simulate various waves sharplybesides, the scheme is able to distinguish small-scale flow structures clearly, and the results solved by the scheme are highly consistent with exact solutions.

     

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