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<journal-id>International Journal of Aerospace and Lightweight Structures</journal-id>
<publication_date>2012</publication_date>
<volume>2</volume>
<issue>2</issue>
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<doi>10.3850/S2010428612000293</doi>
<article-title>Three-point Bending Properties of Composite Lattice Sandwich
Structures with Tetrahedral Truss Cores</article-title>
</title-group>

<author>Jia Lou, Bing Wang ,Li Ma and Linzhi Wu<sup>*</sup></author>
<author-citation>Lou, Jia; Wang, Bing; Ma, Li; Wu, Linzhi</author-citation>

<aff>Center for Composite Materials and Structures, Harbin Institute of Technology, Harbin 150001, PR China.</aff>
<email><a href="mailto:wlz@hit.edu.cn"><sup>*</sup>wlz@hit.edu.cn</a></email>

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<abstract>
<title>ABSTRACT</title>
<p>The mechanical properties of carbon fiber composite lattice sandwich structures with
tetrahedral truss cores under three-point bending are studied in the present paper. Considering
the joint effect of bending of the face sheets and shear of the core, the deflection
response of the sandwich structure is derived. The stresses within the face sheets and
the truss members are calculated respectively, and the corresponding failure modes are
analyzed. Then, collapse mechanism map is conducted to obtain the configuration with
the highest mass efficiency. The entire family of optimized designs of composite lattice
sandwich structures with tetrahedral truss cores is carried out. It is found that the optimized
composite lattice sandwich structures have higher mass efficiency as compared to
metallic lattice sandwich structures and composite solid plates. The structural optimized
design has a guiding significance for engineering.</p><p><italic>Keywords: Composites, Lattice sandwich structures, Three-point bending, Failure modes, Optimized design.</italic></p>
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