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Published in 2020 at "Defence Technology"
DOI: 10.1016/j.dt.2019.07.017
Abstract: Abstract The airborne missile launch mechanism often subjects to significant deformations induced by the large ejection force during high-speed actuations in missile ejection process, leading to a substantial deviation of separation parameters from designed values…
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Keywords:
variable topology;
topology design;
topology;
ejection ... See more keywords