The interaction of on-axis and o -axis laser discharge in front of a hemisphere cylinder in Mach 2.0 ow is investigated numerically. Details of the physics of the interaction of the laser-induced shock and the heated region with the bow shock and its e ect on drag reduction are included. The energetic eciency of the laser discharge in reducing drag is calculated.


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    Title :

    Effect of Off-Body Laser Discharge on Drag Reduction of Hemisphere Cylinder in Supersonic Flow-Part II


    Contributors:

    Conference:

    AIAA SciTech ; 2018 ; Kissimmee, FL, United States


    Publication date :

    2018-01-08


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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    Effect of Off-Body Laser Discharge on Drag Reduction of Hemisphere Cylinder in Supersonic Flow

    Kianvashrad, Nadia / Knight, Doyle D. / Wilkinson, Stephen P. et al. | AIAA | 2017


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