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Trường DCGiá trị Ngôn ngữ
dc.contributor.authorLin, L-
dc.contributor.authorRen, Y X-
dc.contributor.authorHuang, M Y-
dc.contributor.authorZhi, X D-
dc.contributor.authorWang, D Z-
dc.date.accessioned2020-05-30T04:05:14Z-
dc.date.available2020-05-30T04:05:14Z-
dc.date.issued2019-
dc.identifier.issn1687-8086-
dc.identifier.issn1687-8094 (eISSN)-
dc.identifier.otherBBKH1243-
dc.identifier.urihttp://thuvienso.vanlanguni.edu.vn/handle/Vanlang_TV/18521-
dc.descriptionAdvances in Civil Engineering; New York Vol. 2019, (2019). DOI:10.1155/2019/5025637vi
dc.description.abstractSince the 9/11 incident, many engineering research works have been conducted on the impact resistance of large-span space structures. In the present study, a small airplane, Bombardier Challenger 850, was chosen as the test subject. An airplane crash on a single-layered Kiewitt-8 reticulated dome with span 60 m considering roof sheathing effect was simulated using ANSYS/LS-DYNA software. The principles of establishing the numerical model of small airplanes were determined. In addition, the impact styles of small airplane and impact positions on the dome were investigated. The failure modes of reticulated dome with roof sheathing due to small airplane crash were identified. Furthermore, the failure modes between reticulated domes with and without roof sheathing were compared and the effect of roof sheathing on the failure modes of reticulated dome under a small airplane crash was investigated.vi
dc.language.isoenvi
dc.publisherHindawi Limitedvi
dc.subjectAircraft accidentsvi
dc.subjectConstructionvi
dc.subjectAccuracyvi
dc.subjectResearch methodologyvi
dc.subjectTerrorismvi
dc.subjectEngineering researchvi
dc.subjectStudiesvi
dc.subjectFailure modesvi
dc.subjectNumerical modelsvi
dc.titleFailure Modes of a Reticulated Dome in a Small Airplane Crashvi
dc.typeOthervi
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