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dc.contributor.authorZhong, Yuchengen
dc.contributor.authorSuraj, Ravindrababuen
dc.contributor.authorWang, Chenen
dc.contributor.authorChia, Elvin Ser Mingen
dc.contributor.authorJoshi, Sunil Chandrakanten
dc.contributor.authorChen, Zhongen
dc.identifier.citationZhong, Y., Suraj, R., Wang, C., Chia, E. S. M., Joshi, S. C., & Chen, Z. (2018). Damage advancement behavior in braided composite structures for mini aerial vehicles. Mechanics of Advanced Materials and Structures, 25(11), 889-900. doi:10.1080/15376494.2017.1310335en
dc.description.abstractThis work provides a systematic approach to accurately predict damage progression in a composite structure subjected to bending load. Landing gear structures for unmanned aerial vehicles were fabricated from braided textile preforms and assessed for flexural behavior. A multiscale finite element analysis model was developed for analyzing the progressive damage of these structures under bending loads. Microscale and mesoscale analyses were carried out first. Subsequently, the results of microscale and mesoscale analyses were used as inputs in macroscale analyses that predicted the progressive damages in the entire landing gear structure. The numerical results were validated by experimental studies.en
dc.format.extent34 p.en
dc.relation.ispartofseriesMechanics of Advanced Materials and Structuresen
dc.rightsThis is an Accepted Manuscript of an article published by Taylor & Francis in Mechanics of Advanced Materials and Structures on 24 May 2017, available online:
dc.subjectBraided Compositeen
dc.subjectLanding Gearen
dc.titleDamage advancement behavior in braided composite structures for mini aerial vehiclesen
dc.typeJournal Articleen
dc.contributor.schoolSchool of Materials Science & Engineeringen
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen
dc.contributor.researchTemasek Laboratoriesen
dc.description.versionAccepted versionen
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