LAMINATE

作品数:149被引量:146H指数:6
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相关作者:吴敬凯费莲梁震涛孙明琦李子龙更多>>
相关机构:南京航空航天大学中国电子科技集团第十四研究所哈尔滨玻璃钢研究院湖南大学更多>>
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Laminate Tailoring of Composite Tubular Structures to Improve Crashworthiness Design at Off-Axis Loading
《Open Journal of Composite Materials》2018年第3期84-109,共26页A. Rabiee H. Ghasemnejad 
This paper presents experimental and numerical investigation on the parameters effecting energy absorption capability of composite tubular structures at oblique loading to improve crashworthiness performance. Various ...
关键词:CRASHWORTHINESS Composites LAMINATE TAILORING OFF-AXIS OBLIQUE 
Optimum Design for CLD Laminate Plates Using Genetic Algorithms
《Open Journal of Composite Materials》2014年第2期106-116,共11页Guang-Min Luo Tsung-Yen Hsieh 
The optimizations of constrained layered damped (CLD) laminated structures are discussed in this study. Genetic algorithms (GAs) are employed as the search tool for optimization because these algorithms are suitable f...
关键词:Constrained LAYERED DAMPING (Cld) GENETIC Algorithms (Gas) 
Automatic Damage Detection and Monitoring of a Stitch Laminate System Using a Fiber Bragg Grating Strain Sensor
《Open Journal of Composite Materials》2014年第1期47-60,共14页Agus Trilaksono Naoyuki Watanabe Atsushi Kondo Hikaru Hoshi Yutaka Iwahori 
There are numerous aspects and questions related to the use of composite materials for primary structures in aircraft where the structural integrity is the most important factor. This is especially true if the main co...
关键词:Carbon Fiber STITCH LAMINATE DAMAGE TOLERANCE Structural HEALTH MONITORING 
Effects of Boundary Conditions on Postbuckling Strengths of Composite Laminate with Various Shaped Cutouts under In-Plane Shear
《Open Journal of Composite Materials》2013年第2期38-50,共13页Dinesh Kumar Shamsher Bahadur Singh 
Cutouts are often provided in composite structural components for practical reasons. For instance, aircraft components such as wingspar, fuselage and ribs are provided with cutouts for access, inspection, fuel lines a...
关键词:BOUNDARY Conditions BUCKLING POSTBUCKLING Cutouts Composite LAMINATE FEM 
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