A parametric design of ceramic faced composite armor subject to air weapon threats
By taking into consideration the two categories of military projectile threats to aircraft structures, an optimal layer configuration of ceramic faced composite armor was designed in this paper. Using numerical simulations and the same layer arrangement of ceramic, UHMWPE, and carbon fiber laminates...
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| Published in | IOP conference series. Materials Science and Engineering Vol. 103; no. 1; pp. 12017 - 12026 |
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| Main Authors | , |
| Format | Journal Article |
| Language | English |
| Published |
Bristol
IOP Publishing
09.12.2015
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| Subjects | |
| Online Access | Get full text |
| ISSN | 1757-8981 1757-899X |
| DOI | 10.1088/1757-899X/103/1/012017 |
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| Abstract | By taking into consideration the two categories of military projectile threats to aircraft structures, an optimal layer configuration of ceramic faced composite armor was designed in this paper. Using numerical simulations and the same layer arrangement of ceramic, UHMWPE, and carbon fiber laminates, a parametric finite element model using LS-DYNA code was built. Several thickness combinations were analyzed in order to determine the final lightest configuration that is capable of supporting a high-speed impact load and HEI blast wave load, which implements a high anti-penetration design for aircraft armor. This configuration can be used to improve the anti-impact ability of aircraft structures as well as achieve a structure function integration design that considers a lighter weight. |
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| AbstractList | By taking into consideration the two categories of military projectile threats to aircraft structures, an optimal layer configuration of ceramic faced composite armor was designed in this paper. Using numerical simulations and the same layer arrangement of ceramic, UHMWPE, and carbon fiber laminates, a parametric finite element model using LS-DYNA code was built. Several thickness combinations were analyzed in order to determine the final lightest configuration that is capable of supporting a high-speed impact load and HEI blast wave load, which implements a high anti-penetration design for aircraft armor. This configuration can be used to improve the anti-impact ability of aircraft structures as well as achieve a structure/function integration design that considers a lighter weight. |
| Author | Guo, Y N Sun, Q |
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| Cites_doi | 10.1016/j.ijsolstr.2004.07.008 10.1016/0924-0136(95)02050-0 10.1016/j.biomaterials.2003.08.065 10.1063/1.370643 10.1016/0734-743X(90)90035-T 10.1016/j.compstruct.2004.05.014 10.1016/S0734-743X(99)00046-9 |
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| Copyright | Published under licence by IOP Publishing Ltd 2015. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License. |
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| DOI | 10.1088/1757-899X/103/1/012017 |
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| References | Avery J G (1) 1982 12 3 4 Johnson G R (8); 1 5 6 Livermore Software Technology Co. (7) 2007; 1 9 Bergstrom J S (11) 2006 Wilkins M L (2) 1971 10 |
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| SubjectTerms | Aircraft accidents & safety Aircraft components Aircraft configurations Aircraft design Aircraft structures Armor Armor penetration Building codes Carbon fibers Ceramic fibers Ceramics Design engineering Finite element method Impact loads Laminates Mathematical analysis Mathematical models Military aircraft Parametric statistics Polyethylenes Projectiles Weight reduction |
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| Title | A parametric design of ceramic faced composite armor subject to air weapon threats |
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