期刊
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING
卷 33, 期 1-12, 页码 231-243出版社
PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.ijimpeng.2006.09.080
关键词
impact simulation; reinforced carbon-carbon
A series of three dimensional hypervelocity impact simulations has been performed to study the effects of orbital debris impact on the Space Shuttle wing leading edge. The simulations employed an improved hybrid particle-finite element method and an orthotropic elastic-plastic material model recently developed for reinforced carbon-carbon. The simulation results are consistent with the available experimental data, and suggest the use of momentum scaling to estimate damage effects for impact conditions outside the range of current light gas gun technology. Projectile shape and orientation effects appear to be modest for flat plate projectiles at impact velocities above the ballistic limit. (C) 2006 Elsevier Ltd. All rights reserved.
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