Failure mechanisms of impact-damaged sandwich panels under uniaxial compression-Reference-Cited by-同舟云学术

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Failure mechanisms of impact-damaged sandwich panels under uniaxial compression

Published:1994-04-18 Issue: Volume: Page:
ISSN:
Container-title:35th Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

Tsang P.¹,Lagace Paul¹

Affiliation:

1. MIT, Cambridge, MA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-1396

Reference29 articles.

1. Services,1989,pp. 3-22.

2. India,Vol.43,No.2,May, 1991,pp. 101-112.

3. Reno,NV, 1989,pp. 824-838.

Cited by 8 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

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2. Residual compressive strength of aluminum alloy honeycomb sandwich panel in the presence of multiple impact dents;Journal of Sandwich Structures & Materials;2021-08-01

3. An experimental and numerical investigation of core damage size in honeycomb sandwich panels subject to low-velocity impact;Composite Structures;2020-12

4. Compression After Impact Experiments on Thin Face Sheet Honeycomb Core Sandwich Panels;Journal of Spacecraft and Rockets;2014-01

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