The response of honeycomb sandwich panels under low-velocity impact loading-Reference-Cited by-同舟云学术

The response of honeycomb sandwich panels under low-velocity impact loading

Published:2005-09 Issue:9 Volume:47 Page:1301-1325
ISSN:0020-7403
Container-title:International Journal of Mechanical Sciences
language:en
Short-container-title:International Journal of Mechanical Sciences

Author:

Meo M.,Vignjevic R.,Marengo G.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science,Civil and Structural Engineering

Reference69 articles.

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3. McGowan DM, Ambur DR. Compression Response of a Sandwich Fuselage Keel Panel With and Without Damage. NASA Technical Memorandum 110302.

4. McGowan DM, Ambur DR. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. NASA Technical Memorandum 110303.

5. Rouse M, Ambur DR, Bodine J, Dopker B. Evaluation of a composite sandwich fuselage side panel with damage and subjected to internal pressure. NASA Technical Memorandum 110309.

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