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전체 선택해제
총 99건 검색
본문검색 결과만 보기
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Comparative numerical evaluation for the low velocity impact behavior of T300 and T800 composite system
Jae-Seok Choi, Heung Soap Choi, Soo-Jin Park, Myung Kyun Park 한국탄소학회 Carbon Letters 7 Pages
한국탄소학회 Carbon Letters 2017, Vol.22 9 89-95 (7 pages)
Carbon fiber reinforced polymer (CFRP) composites have been used for many decades for extreme light weight design purposes in various areas, such as the aerospace industry, automobiles, sports goods and etc. because they provide the advantages of high specific strength and high rigidity [1]. In particular, the fuselage and wings of various aircraft, as well as the load bearing structures and components of mechanical and civil engineering systems are currently being manufactured with CFRP.... -
Disorientation angle influence on the thermal residual stresses in carbon multilayered composite plates of different thicknesses
Olga Bitkina, Ki-Weon Kang, Jang-Ho Lee 한국탄소학회 Carbon Letters 5 Pages
한국탄소학회 Carbon Letters 2017, Vol.21 13 98-102 (5 pages)
One of the most acute problems in studying composite stress-strain states is determining the initial residual stresses during the design of layered construction elements. The full stress?strain state of composite constructions consists of the initial (generated during the manufacturing process) and operating (generated during the working period) stages. A thorough investigation of the initial stage of the stress-strain state is very important to finding the total stresses and deformations, and... -
The effects of stacking sequence on the penetration-resistant behaviors of T800 carbon fiber composite plates under low-velocity impact loading
Furqan Ahmad, Jung-Wuk Hong, Heung Soap Choi, Soo-Jin Park, Myung Kyun Park 한국탄소학회 Carbon Letters 9 Pages
한국탄소학회 Carbon Letters 2015, Vol.16 No.2 6 107-115 (9 pages)
the CFRP composite plates were significantly affected by the laminate stacking sequences. Three types of specimens, specifically quasi-isotropic, unidirectional, and cross-ply, were tested by a constant impact carrying the same impact energy level. An impact load of 3.44 kg, corresponding to 23.62 J, was applied to the center of each plate supported at the boundaries. The unidirectional composite plate showed the worst impact resistance and broke completely into two parts; this was followed by... -
Evaluation of Tension-Compression and Tension-Tension Fatigue Life of Woven Fabric Glass/Epoxy Laminate Composites used in Railway Vehicle
Jeon. Kwang-Woo, Shin. Kwang-Sok, Kim. Jung-Seok 한국정밀공학회 International journal of precision engineering and manufacturing 8 Pages
한국정밀공학회 International journal of precision engineering and manufacturing 2011, Vol.12 No.5 813-820 (8 pages)
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Tension-Compression Asymmetry in the Off-Axis Nonlinear Rate-Dependent Behavior of a Unidirectional Carbon/Epoxy Laminate at High Temperature and Incorporation into Viscoplasticity Modeling
Kawai. M., Zhang. J.Q., Saito. S., Xiao. Y., Hatta. H. 한국복합재료학회 Advanced composite materials : the official journal of the Japan Society of Composite Materials and 21 Pages
한국복합재료학회 Advanced composite materials : the official journal of the Japan Society of Composite Materials and 2009, Vol.18 No.3 265-285 (21 pages)
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Tensile strength of unidirectional CFRP laminate under high strain rate
Taniguchi. Norihiko, Nishiwaki. Tsuyoshi, Kawada. Hiroyuki 한국복합재료학회 Advanced composite materials : the official journal of the Japan Society of Composite Materials and 14 Pages
한국복합재료학회 Advanced composite materials : the official journal of the Japan Society of Composite Materials and 2007, Vol.16 No.2 167-180 (14 pages)
