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Numerical simulations of low-velocity impact on an aircraft sandwich panel
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What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.1016/0010-4361(83)90020-4openalex-snapshot
Post-impact fatigue performance of carbon fibre laminates with non-woven and mixed-woven layers
inferredcites →https://doi.org/10.1115/1.3101689openalex-snapshot
Localized Impact on Sandwich Structures With Laminated Facings
inferredcites →https://doi.org/10.1115/1.3111065openalex-snapshot
Impact on Laminated Composites: Recent Advances
inferredcites →https://doi.org/10.1115/1.3119500openalex-snapshot
Impact on Laminated Composite Materials
inferredcites →https://doi.org/10.1177/002199838702100904openalex-snapshot
A Progressive Damage Model for Laminated Composites Containing Stress Concentrations
inferredcites →https://doi.org/10.1177/002199839202601408openalex-snapshot
A Model for Predicting Damage in Graphite/Epoxy Laminated Composites Resulting from Low-Velocity Point Impact
inferredcites →https://doi.org/10.2514/1.22397openalex-snapshot
Response of Composite Fuselage Sandwich Side Panels Subjected to Internal Pressure and Axial Tension
inferredcites →https://doi.org/10.2514/6.1991-1075openalex-snapshot
A model for predicting the behavior of impact-damaged minimum gage sandwich panels under compression
inferredcites →https://doi.org/10.2514/6.1998-1708openalex-snapshot
Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension
inferredcites →https://doi.org/10.2514/6.1998-1783openalex-snapshot
Damage characteristics and residual strength of composite sandwich panels impacted with and without a compression loading
What points at this work
Incoming claims: where this work appears in other papers’ reference lists and arguments.
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