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.
Effect of Off-Body Laser Discharge on Drag Reduction of Hemisphere Cylinder in Supersonic Flow-Part II
AIAA SciTech ; 2018 ; Kissimmee, FL, United States
2018-01-08
Conference paper
No indication
English
British Library Conference Proceedings | 2018
|Hemisphere-Cylinder in Low Supersonic Flow
AIAA | 1975
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