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Instability of Metamaterial-Based Thin Cylindrical Shells Under Axial Compression
Mitansh Doshi,
Xin Ning
Aerospace Engineering
Materials Research Lab
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Keyphrases
Metamaterials
100%
Axial Compression
100%
Cylindrical Shell
100%
Thin Cylindrical Shell
100%
Post-buckling Behavior
33%
Structural Mass
33%
Mass Efficiency
33%
Critical Buckling Load
33%
Cylindrical Metamaterials
33%
Octahedron
16%
Quadratic Relation
16%
Defect Effect
16%
Cuboid
16%
Post-buckling
16%
Behavioral Effects
16%
Axial Load
16%
Continuous Surface
16%
Instability Behavior
16%
Shell Dimensions
16%
Octet-truss
16%
Multistable
16%
Metamaterial Unit Cell
16%
Engineering
Axial Compression
100%
Cylindrical Shell
100%
Buckling Behavior
28%
Critical Buckling Load
28%
Numerical Study
14%
Axial Load
14%
Dimensional Variation
14%