Numerical analysis of vortex breakdown of unmanned combat air vehicles
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Abstract (EN)
In this study, vortex breakdown of different unmanned combat air vehicles is investigated by using numerical methods with various angle of attacks. Also streamline topology of wings are investigated by taking results from a section plane and they are compared with available experimental results in the literature. Particle injection technique is used for displaying of vortex formation and breakdown. As a result of applied analysis, it?s determined that the vortex formation is directly influenced by the change of angle of attack and further increments of angle of attack of 170, vortex formation takes a critical condition
Author
Mustafa Murat Yavuz
How to Cite
Mustafa Murat Yavuz (Master Thesis). Numerical analysis of vortex breakdown of unmanned combat air vehicles, 2011, Çukurova University.
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