Volume 37 Issue 8
Sep 2022
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LI Junhong,LÜ Junming,MIAO Wenbo,et al.Real gas effects on the plasma sheath and the electromagnetic parameters of the reentry vehicle[J].Journal of Aerospace Power,2022,37(8):1579‑1586. doi: 10.13224/j.cnki.jasp.20210124
Citation: LI Junhong,LÜ Junming,MIAO Wenbo,et al.Real gas effects on the plasma sheath and the electromagnetic parameters of the reentry vehicle[J].Journal of Aerospace Power,2022,37(8):1579‑1586. doi: 10.13224/j.cnki.jasp.20210124

Real gas effects on the plasma sheath and the electromagnetic parameters of the reentry vehicle

doi: 10.13224/j.cnki.jasp.20210124
  • Received Date: 19 Mar 2021
    Available Online: 06 Sep 2022
  • Issue Publish Date: 28 Aug 2022
  • The numerical simulation technology of thermochemical non⁃equilibrium flow was established for aircraft hypersonic flight environment,the reliability of the calculation method was verified,and the influence law of high temperature real gas effect on plasma sheath and electromagnetic parameters in plasma was analyzed.The results showed:the numerical calculation results of aircraft peak plasma density on wall central line were in agreement with flight test results,as for the collision frequency,along the stagnation line,the two⁃temperature model and the Park reaction model had the same influence trend on the plasma collision frequency;for the relative dielectric constant,near the shock wave,the real part of other areas of the flow field was close to 1,and the imaginary part gradually increased along the stagnation line;The influence trend of the two⁃temperature model and the Park reaction model on the real and imaginary parts of the relative dielectric constant were consistent.

     

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