Multidisciplinary design optimization of long-range slender guided rockets considering aeroelasticity and subsidiary loads
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DOI: 10.1016/j.ast.2019.06.039
Abstract: Abstract Due to the insufficient rigidity feature and long-range requirement, it is crucial to consider the aeroelasticity and subsidiary loads caused by the Earth rotation and fuel consumption when designing long-range slender guided rockets (LRSGRs).… read more here.
Keywords: optimization; aeroelasticity; subsidiary loads; long range ... See more keywords