期刊
ENGINEERING STRUCTURES
卷 175, 期 -, 页码 895-911出版社
ELSEVIER SCI LTD
DOI: 10.1016/j.engstruct.2018.08.082
关键词
Continuum mechanics; Blast actions; Shock waves; Explosions; Aircrafts
We introduce a numerical approach for evaluating the behaviour of aircraft fuselages subjected to internal explosions. At variance with available approaches, we consider fluid-structure interactions through a novel integrated methodology able to take into account both stress at cruise altitude and blast fast-dynamics in interaction with pressurization not considered as a static load. The precision of the proposed numerical procedure allows us to foresee a nonstandard composite protective device.
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