Design and performance of novel aircraft structures with folded composite cores-Reference-Cited by-同舟云学术

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Design and performance of novel aircraft structures with folded composite cores

Published:2015 Issue: Volume: Page:793-827
ISSN:
Container-title:Structural Integrity and Durability of Advanced Composites
language:
Short-container-title:

Author:

Johnson A.,Kilchert S.,Fischer S.,Toso-Pentecôte N.

Publisher

Elsevier

Reference44 articles.

1. Localized impact on sandwich structures with laminated facings;Abrate;Applied Mechanics Reviews,1997

2. Impact on composite structures;Abrate,1998

3. Dynamic failure of composite and sandwich structures,2013

4. Prediction of impact damage on sandwich composite panels;Aktay;Computational Materials Science,2005

5. Experimental investigation of low-velocity impact characteristics of sandwich composites;Anderson;Composite Structures,2000

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1. The energy absorption capacity of a novel dual-sub-fold Miura foldcore subjected to axial crushing;Materials & Design;2024-07

2. Rapid prototyping of core materials in aircraft sandwich structures;Modern Manufacturing Processes for Aircraft Materials;2024

3. Energy Absorption of a Novel Dual-Defect Miura Foldcore Subject to Quasi-Static Axial Crushing;2023

4. Low-velocity impact response and damage phenomena of hybrid S-shaped folded sandwich structure;Thin-Walled Structures;2022-12

5. Experimental and numerical research on the dynamic response of sandwich structure with M-type foldcore under low-velocity impact;Mechanics of Advanced Materials and Structures;2022-12-01

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