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Published in 2020 at "AIAA Journal"
DOI: 10.2514/1.j059689
Abstract: We present experiments and simulations of plunging maneuvers of large amplitude, for velocity ratios of G=1 and 2, defined as the ratio between the peak plunge velocity and the freestream velocity....
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Keywords:
wings plunge;
forces wings;
aerodynamic forces;
characterization aerodynamic ... See more keywords