• Infrared and Laser Engineering
  • Vol. 46, Issue 2, 211001 (2017)
Li Ming, Zhu Zhiwei, Yang Yanguang, and Xie Aimin
Author Affiliations
  • [in Chinese]
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    DOI: 10.3788/irla201746.0211001 Cite this Article
    Li Ming, Zhu Zhiwei, Yang Yanguang, Xie Aimin. Flow visualization using double-pass schlieren technique in hypersonic flow[J]. Infrared and Laser Engineering, 2017, 46(2): 211001 Copy Citation Text show less
    References

    [1] Wang Diankai, Hong Yanji, Li Qian, et al. Color schlieren for hypersonic shock wave structures[J]. Infrared and Laser Engineering, 2014, 43(6): 1710-1714. (in Chinese)

    [2] Yu Kaikai, Xu Jinglei, Tang Lan, et al. Density measurements of nozzle under over-expanded condition using background oriented schlieren technique [J]. Journal of Propulsion Technology, 2015, 36(6): 832-838. (in Chinese)

    [3] Ye Jifei, Hong Yanji. Quantitative measurement of density by color schlieren based on axial symmetry field[J]. Infrared and Laser Engineering, 2014, 43(12): 3335-3338. (in Chinese)

    [4] Meng Sheng,Yang Zangjian,Wang Mingxiao. Application of quantitative schlieren method in flame temperature measurement[J]. Journal of Experiments in Fluid Mechanics, 2015, 29(4): 65-69. (in Chinese)

    [5] Lukasiewicz J. Hypersonic Experimental Method[M]. Beijing: National Defence Industrial Press, 2006: 481-482.(in Chinese)

    [6] Yang Zuqing. Flow Visualization Technique[M]. Beijing: National Defence Industrial Press, 2002: 105-131. (in Chinese)

    [7] Li Guichun. Aero-Optics[M]. Beijing: National Defence Industrial Press, 2006: 411-415. (in Chinese)

    [8] Gottlleb J. Evaluation of a double-pass schlieren system[G]. Suffield Memorandum, 1968: 54-67.

    Li Ming, Zhu Zhiwei, Yang Yanguang, Xie Aimin. Flow visualization using double-pass schlieren technique in hypersonic flow[J]. Infrared and Laser Engineering, 2017, 46(2): 211001
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