Analysis of Vortex on Sharp-Edged Delta Wing With Blowing Effect
Muhammad Faris Aqil Zamzuddin,
Mazuriah Said,
Nur Amalina Musa
et al.
Abstract:The formation of the primary vortex above the wing is dependent on the Reynolds number, the angle of attack, the Mach number, and the bluntness of the leading edge. This experiment is done in order to assess the impacts of blowing at three sites on the delta wing's flow topology. The blower was placed on the leading edge at the 15%, 50%, and 70% wing sections. The experiment was conducted at a Reynolds number of 8 x 105, which corresponds to a wind speed of 25 m/s and a mean aerodynamic chord. The UTM generic … Show more
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