Infrared and Laser Engineering, Volume. 48, Issue 8, 809001(2019)

Study on correction method of aero-optical effects caused by supersonic mixing layer based on flow control

Guo Guangming*
Author Affiliations
  • [in Chinese]
  • show less

    The periodic controlled supersonic mixing layer was simulated using large eddy simulation(LES) method. Features of vortices in this flow field was revealed clearly, and the ray tracing method was employed to calculate wave front distortion of a beam passing through the controlled supersonic mixing layer. A correction method for wave front distortion was proposed based on the analysis of dynamical characteristic of vortices in the controlled flow field, and it was tested by a supersonic mixing layer periodic controlled with different frequencies. The results show that the presented correction method can reduce the amplitude of wave front distortion to 50 percent or more, and shape of the controlled vortex in mixing layer is the key factor dominating the correction effect.

    Tools

    Get Citation

    Copy Citation Text

    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

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Save article for my favorites
    Paper Information

    Category: 大气光学

    Received: Mar. 11, 2019

    Accepted: Apr. 21, 2019

    Published Online: Sep. 3, 2019

    The Author Email: Guangming Guo (guoming20071028@163.com)

    DOI:10.3788/irla201948.0809001

    Topics