CONSTITUTIVE MODEL AND DYNAMIC MECHANICAL PROPERTIES OF GLASS-CLOTH/EPOXY LAMINATES AT DIFFERENT TEMPERATURES
CONSTITUTIVE MODEL AND DYNAMIC MECHANICAL PROPERTIES OF GLASS CLOTH/EPOXY LAMINATES AT DIFFERENT TEMPERATURES
摘要
CONSTITUTIVEMODELANDDYNAMICMECHANICALPROPERTIESOFGLASS┐CLOTH/EPOXYLAMINATESATDIFFERENTTEMPERATURESHANXiaoping(韩小平)1,HANShenli...
-
1Kou Changhe,LuMeng,LinFeng(Beijing University of Aeronautics and Astronautics, Beijing, China, 100083).CREEP BEHAVIOUR OF T300/5222(C/E)COMPOSITE LAMINATEWITH CROSS-PLY[J].Chinese Journal of Aeronautics,1994,7(4):276-282.
-
2Yang Xianjie(Southwest Jiaotong University)Chengdu,China,610031.CYCLIC VISCOPLASTIC DESCRIPTION FOR THE MEAN STRAIN EFFECT[J].Chinese Journal of Aeronautics,1995,8(2):111-117.
-
3Zhang Yong,Zhang Shaoqing,Tao Chunhu(Institute of Aeronautical Materials, Beijing, China, 100095).EFFECTS OF STRAIN RATE & TEMPERATURE ON HOT COMPRESSION FLOW BEHAVIOR OF A HYDROGENATED CAST Ti-25Al-10Nb-3V-1Mo ALLOY[J].Chinese Journal of Aeronautics,1996,9(2):130-134.
-
4刘晓辉,黄英,李郁忠.编织物增强层板的抗冲击性研究[J].兵器材料科学与工程,1998,21(6):12-16. 被引量:1
-
5Dayang Laila Abang Haji Abdul Majid,ShahNor Basri.LCO flutter of cantilevered woven glass/epoxy laminate in subsonic flow[J].Acta Mechanica Sinica,2008,24(1):107-110.
-
6郭亚军,吴学仁.FACTORS AFFECTING FATIGUE CRACK GROWTH RATES OF FIBER REINFORCED METAL LAMINATES[J].Chinese Journal of Aeronautics,1998,11(2):73-77.
-
7刘丹梅,曲伟,杨为奉,张瑞平,夏月波.玻璃纤维-Al 混杂复合层板的疲劳裂缝扩展行为[J].材料科学进展,1992,6(5):450-454.
-
8Zhong Weihong,Chen Changqi,Kou Changhe (Beijing University of Aeronautics and Astronautics, Beijing, China, 100083)Zheng Ruiqi (Beijig Institute of Aeronautical Materials, Beijing, China, 100095).EXPERIMENTAL STUDY OF EFFECTS ON DELAMINATION NEAR CRACK OF ARALL BY RESIDUAL STRESS UNDER FATIGUE & STATIC LOADS[J].Chinese Journal of Aeronautics,1996,9(3):211-216.
-
9Li Hongyun,Hu Hongiun,Zheng Rulqi(Beijing institute of Aeronautical Materials, Beijing, China, 100095).ANALYSIS AND MEASUREMENT ONRESIDUAL STRESS OF ARAMIDALUMINIUMLAMINATE[J].Chinese Journal of Aeronautics,1994,7(4):283-288.
-
10Liang Dakai,Tao Baoqi(Sensoring and Testing Research institute, Naming University of Aeronautics and Astronautics, Nanjing, China, 210016).STRAIN MEASUREMENT IN THE SMART COMPOSITE[J].Chinese Journal of Aeronautics,1996,9(1):55-63.