High-velocity impact loading in honeycomb sandwich panels reinforced with polymer foam: a numerical approach study
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Title
High-velocity impact loading in honeycomb sandwich panels reinforced with polymer foam: a numerical approach study
Authors
Keywords
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Journal
IRANIAN POLYMER JOURNAL
Volume 29, Issue 8, Pages 707-721
Publisher
Springer Science and Business Media LLC
Online
2020-06-05
DOI
10.1007/s13726-020-00833-5
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- Crashworthiness design optimisation of metal honeycomb energy absorber used in lunar lander
- (2011) Meng Li et al. INTERNATIONAL JOURNAL OF CRASHWORTHINESS
- Comparisons of honeycomb sandwich and foam-filled cylindrical columns under axial crushing loads
- (2011) Zonghua Zhang et al. THIN-WALLED STRUCTURES
- Modelling of composite sandwich structures with honeycomb core subjected to high-velocity impact
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- Analysis of structural performance of sandwich plates with foam-filled aluminum hexagonal honeycomb core
- (2008) Vyacheslav N. Burlayenko et al. COMPUTATIONAL MATERIALS SCIENCE
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- (2008) K.S. Raju et al. JOURNAL OF COMPOSITE MATERIALS
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