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Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.01.002
Abstract: Abstract This study investigates the flow structures and aerodynamic performance of a slender delta wing that has a sweep angle of 65 degrees and is equipped with acicular vortex generators. The results were compared with…
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Keywords:
acicular vortex;
vortex generators;
delta wing;
slender delta ... See more keywords