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Published in 2023 at "Journal of Aircraft"
DOI: 10.2514/1.c037186
Abstract: Ways to maximize the lift-to-drag ([Formula: see text]) and the thrust-to-drag ([Formula: see text]) ratios of hypersonic vehicles are computed using the reduced-order model Michigan-AFRL Scramjet in Vehicle (MASIV). The 84 geometries considered are variations…
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Keywords:
formula see;
hypersonic vehicles;
thrust drag;
see text ... See more keywords