Hypervelocity Impact On Spacecraft Honeycomb: Hydrocode Simulation And Damage Laws-Reference-Cited by-同舟云学术

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Hypervelocity Impact On Spacecraft Honeycomb: Hydrocode Simulation And Damage Laws

Published:2003-12 Issue:1-10 Volume:29 Page:691-702
ISSN:0734-743X
Container-title:International Journal of Impact Engineering
language:en
Short-container-title:International Journal of Impact Engineering

Author:

Taylor Emma A.,Glanville Jonathan P.,Clegg Richard A.,Turner Robert G.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Safety, Risk, Reliability and Quality,Aerospace Engineering,Automotive Engineering,Civil and Structural Engineering

Cited by 40 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. Damage effects of aluminum alloy honeycomb sandwich panel double-layer structure induced by reactive projectile hypervelocity impact;Thin-Walled Structures;2024-09

3. Review of bumper materials for spacecraft shield against orbital debris hypervelocity impact;Defence Technology;2024-09

4. Load-bearing behaviors of sandwich plates with non-uniformly distributed grid cores: Dynamic impact and blast;Materials Today Communications;2024-08

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