Abstract
AbstractIn order to visualize the rarefied flow field in a Φ1m hypersonic low-density wind tunnel, an electric glow discharge technique based on high frequency excited power has been developed. Firstly, finite element simulation analysis has been carried out, and it is concluded that the breakdown voltage can be reduced by using high frequency power supply; then an electric glow discharge apparatus has been fabricated, and the discharge images were compared with simulations; besides, a clear flow field around HB-1 standard model has been observed using this technology; finally, the influence of glow discharge on the flow field, as well as the differences between direct current and high frequency electric glow discharges is discussed at the end of this paper.
Publisher
Springer Science and Business Media LLC
Reference27 articles.
1. Merzkirch W (1987) Flow visualization, 2nd edn. Academic Press, Orlando
2. Freymuth P (1993) Flow visualization in fluid mechanics. Rev Sci Instrum 64(1):1–18. https://doi.org/10.1063/1.1144433
3. Estruch D, Lawson NJ, Garry KP (2009) Application of optical measurement techniques to supersonic and hypersonic aerospace flows. J Aerosp Eng 22(4):383–395. https://doi.org/10.1061/(ASCE)0893-1321(2009)22:4(383)
4. Kunnel WB, Hurlbut FC (1957) Luminescent gas flow visualization for low density wind tunnels. J Appl Phys 28:827–835
5. Liu D, Baccarella D, Lee T (2017) Investigation of flow combustion dynamics of an ethylene transverse jet in a model scramjet. In: 55th AIAA aerospace sciences meeting, Grapevine, Texas, pp 2017–0341
Cited by
3 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献