• Infrared and Laser Engineering
  • Vol. 48, Issue 8, 809001 (2019)
Guo Guangming*
Author Affiliations
  • [in Chinese]
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    DOI: 10.3788/irla201948.0809001 Cite this Article
    Guo Guangming. Study on correction method of aero-optical effects caused by supersonic mixing layer based on flow control[J]. Infrared and Laser Engineering, 2019, 48(8): 809001 Copy Citation Text show less
    References

    [1] Yin Xingliang. Principle of Aero-optics [M]. Beijing: China Astronautics Press, 2003: 2. (in Chinese)

    [2] Wang Naixiang, Xu Yulei, Shi Lei, et al. Analysis of the impact of windward and angle of attack to the flow field around the optical window on high Mach condition [J]. Infrared and Laser Engineering, 2015, 44(4): 1267-1272. (in Chinese)

    [3] Ding Haolin, Yi Shihe, Wu Yuyang, et al. Investigation on correction method of aero-optical transmission effects imaging deviation based on BOS technique [J]. Infrared and Laser Engineering, 2018, 47(4): 0418003. (in Chinese)

    [4] Jumper E J, Hugo R J. Quantification of aero-optical phase distortion using the small-aperture beam technique[J]. AIAA Journal, 1995, 33(11): 2151-2157.

    [5] Catrakis H J, Aguirre R C. New interfacial fluid thickness approach in aero-optics with applications to compressible turbulence[J]. AIAA Journal, 2004, 42(10): 1973-1981.

    [6] Dimotaksi P, Catrakis H, Fourguette D. Flow structure and optical beam propagation in high-reynolds-number gas-phase shear layers and jets[J]. Journal of Fluid Mechanics, 2001, 433: 105-143.

    [7] Gan Caijun, Li Lang, Ma Handong, et al. Theoretical and experimental investigations on aero-optical effect of the compressible mixing layer[J]. Acta Physica Sinica, 2014, 63: 054703. (in Chinese)

    [8] Guo G M, Liu H, Zhang B. Development of a temporal evolution model for aero-optical effects caused by vortices in the supersonic mixing layer[J]. Applied Optics, 2016, 55(10): 2708-2717.

    [9] Visbal M R, Rizzeta D P. Effect of flow excitation on aero-optical aberration [C]//44th AIAA Aerospace Science Meeting and Exhibit, 2008: 1074.

    [10] Rennie R M, Siegenthaler J P, Jumper E J. Forcing of a two- dimensional, weakly-compressible subsonic free shear layer [C]//44th AIAA Aerospace Science Meeting and Exhibit, 2006: 561.

    [11] Rennie R M, Duffin D A, Jumper E J. Characterization of a Forced two- dimensional, weakly-compressible subsonic free shear layer [C]//38th AIAA Aerospace Science Meeting and Exhibit, 2007: 4007.

    [12] Freeman A P, Catrakis H J. Direct reduction of aero-optical aberrations by large structure suppression control in turbulence [J]. AIAA Journal, 2008, 46(10): 2582-2590.

    [13] Guo Guangming, Liu Hong, Zhang Bin, et al. Characteristics of convective speeds of vortex structures in mixing layer [J]. Acta Physica Sinica, 2016, 65(7): 074702. (in Chinese)

    [14] Guo G M, Liu H, Correcting aero-optical wavefront aberration of the supersonic mixing layer based on periodic pulse forcing [J]. Applied Optics, 2017, 56(16): 4613-4621.

    [15] Ravindraan S S. Reduced-order adaptive controllers for fluids using proper orthogonal decomposition[C]//9th AIAA Aerospace Sciences Meeting and Exhibit, 2001: 0925.

    Guo Guangming. Study on correction method of aero-optical effects caused by supersonic mixing layer based on flow control[J]. Infrared and Laser Engineering, 2019, 48(8): 809001
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