Crush energy absorption of composite channel section specimens
Carbon/epoxy square tubes and channel sections have been used in modern automotive and aircraft structures, respectively, as dedicated components designed to dissipate energy under controlled collapse. However, there are currently no specialized test methods for the characterization of Specific Ener...
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Published in | Composites. Part A, Applied science and manufacturing Vol. 40; no. 8; pp. 1248 - 1256 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
Kidlington
Elsevier Ltd
01.08.2009
Elsevier |
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Online Access | Get full text |
ISSN | 1359-835X 1878-5840 |
DOI | 10.1016/j.compositesa.2009.05.021 |
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Abstract | Carbon/epoxy square tubes and channel sections have been used in modern automotive and aircraft structures, respectively, as dedicated components designed to dissipate energy under controlled collapse. However, there are currently no specialized test methods for the characterization of Specific Energy Absorption (SEA) of composite materials. A systematic experimental investigation is conducted to evaluate the effect of geometric features on crush behavior. From a square tube, individual test segments are machined in order to isolate corner radii and flat sections of varying sizes, for a total of five different test geometries. Laminate thickness, material system, manufacturing process, and test methodology are kept constant throughout the study. For the material system and lay-up considered in this study, fiber tensile fracture and tearing at the corners is responsible for the vast percentage of the energy absorbed, while frond formation and splaying of the flat segments is responsible for a much lower percentage. An analytical expression is derived that accounts for the combined behavior of corner elements and flat segments in the crush behavior of more complex test articles, such as tubes. |
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AbstractList | Carbon/epoxy square tubes and channel sections have been used in modern automotive and aircraft structures, respectively, as dedicated components designed to dissipate energy under controlled collapse. However, there are currently no specialized test methods for the characterization of Specific Energy Absorption (SEA) of composite materials. A systematic experimental investigation is conducted to evaluate the effect of geometric features on crush behavior. From a square tube, individual test segments are machined in order to isolate corner radii and flat sections of varying sizes, for a total of five different test geometries. Laminate thickness, material system, manufacturing process, and test methodology are kept constant throughout the study. For the material system and lay-up considered in this study, fiber tensile fracture and tearing at the corners is responsible for the vast percentage of the energy absorbed, while frond formation and splaying of the flat segments is responsible for a much lower percentage. An analytical expression is derived that accounts for the combined behavior of corner elements and flat segments in the crush behavior of more complex test articles, such as tubes. |
Author | Wade, Bonnie Feraboli, Paolo Deleo, Francesco Rassaian, Mostafa |
Author_xml | – sequence: 1 givenname: Paolo surname: Feraboli fullname: Feraboli, Paolo email: feraboli@u.washington.edu organization: Department of Aeronautics and Astronautics, University of Washington, Seattle, WA, United States – sequence: 2 givenname: Bonnie surname: Wade fullname: Wade, Bonnie organization: Department of Aeronautics and Astronautics, University of Washington, Seattle, WA, United States – sequence: 3 givenname: Francesco surname: Deleo fullname: Deleo, Francesco organization: Department of Aeronautics and Astronautics, University of Washington, Seattle, WA, United States – sequence: 4 givenname: Mostafa surname: Rassaian fullname: Rassaian, Mostafa organization: Advanced Structures Technology, Boeing Phantom Works, Seattle, WA, United States |
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Keywords | D. Mechanical testing B. Fragmentation A. Carbon fibre B. Impact behavior Tube Stacking sequence Laminate Mechanical model Unidirectional fiber material Fiber reinforced material Epoxy resin Mechanical properties Experimental study Mineral fiber Modeling Composite material Impact strength Square shape Energy absorption Crush Fracture mode Carbon fiber |
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SubjectTerms | A. Carbon fibre Applied sciences B. Fragmentation B. Impact behavior D. Mechanical testing Exact sciences and technology Forms of application and semi-finished materials Laminates Polymer industry, paints, wood Technology of polymers Tubes |
Title | Crush energy absorption of composite channel section specimens |
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