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Published in 2019 at "AIAA Journal"
DOI: 10.2514/1.j058284
Abstract: A numerical study has been conducted to investigate the unsteady nature of afterbody vortices shed from an upswept region of a simple fuselage configuration. The upsweep angle considered is ϕ=28 d...
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Keywords:
simulations afterbody;
vortex flows;
high fidelity;
afterbody vortex ... See more keywords