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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2023
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Article
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Tab 1
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Research Article
A Modified Strain-Rate-Dependent Spring-Mass Model for Response Prediction of Composite Laminates Subjected to Low-Velocity Impact
Table 1
Expressions of
,
,
and
with different boundary conditions.
Boundary conditions
Edge-moveable clamped
Edge-immoveable clamped
Edge-moveable simple-supported
Edge-immoveable simple-supported