Please use this identifier to cite or link to this item: http://hdl.handle.net/123456789/25047
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dc.contributor.authorAbdul Rauf Abdul Raif-
dc.contributor.authorMuhammed Fadzli Ismail-
dc.contributor.authorMulia Minhat-
dc.date.accessioned2021-07-17T03:20:05Z-
dc.date.available2021-07-17T03:20:05Z-
dc.date.issued2019-
dc.identifier.citationRaif, A.R.A.,Ismail, M.F.,Minhat, M. 2nd International Conference of Aerospace and Mechanical Engineering, AeroMech 2019; Seberang Perai; Malaysia; 20 November 2019 through 21 November 2019; Code 241099, 2020, Pages 177-190, Lecture Notes in Mechanical Engineering, DOI: 10.1007/978-981-15-4756-0_16en_US
dc.identifier.isbn978-981154755-3-
dc.identifier.issn21954356-
dc.identifier.urihttp://hdl.handle.net/123456789/25047-
dc.description.abstractEshelby integral formula, which was initially derived for a single inclusion embedded in all matrix system, plays a fundamental role in the micromechanics of composite or heterogeneous materials. The integral formula is remarked to be readily generalized to the case of multiple inclusions. However, the proof for such case has never been established. Herein, the integral formula is reformulated within the frameworks of generalized self-consistent method for the case of multiple inclusion composite system and thus, establishing the proof of its generalized version. © Springer Nature Singapore Pte Ltd 2020.en_US
dc.language.isoen_USen_US
dc.publisherSpringer, Singaporeen_US
dc.subjectEshelby integral formulaen_US
dc.subjectGeneralized self-consistent methoden_US
dc.subjectMultiphase compositesen_US
dc.subjectMultiple inclusionen_US
dc.titleGeneralized eshelby integral formula for multiple inclusion composite materialsen_US
dc.typeWorking Paperen_US
dc.conference.name2nd International Conference of Aerospace and Mechanical Engineering, AeroMech 2019en_US
dc.conference.year2019en_US
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