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作 者:刘智敏 孙启星 刘慧慧 毛端华 王艳丽 朱丽媛 Liu Zhimin;Sun Qixing;Liu Huihui;Mao Duanhua;Wang Yanli;Zhu Liyuan(Air Force Representative Office,Nanchang,Jiangxi 330024;AVIC-Hongdu,Nanchang,Jiangxi 330024)
机构地区:[1]空军驻江西地区军事代表室,江西南昌330024 [2]航空工业洪都,江西南昌330024
出 处:《教练机》2018年第3期65-68,共4页Trainer
摘 要:对复合材料加筋壁板进行了试验和理论分析,其计算结果与试验吻合良好,在此基础上进行了线性和几何非线性对比分析,结果表明,几何非线性可提高加筋壁板刚度18.2%和强度19.1%,通过对比线性结果和几何非线性计算结果可知,结构的刚度、结构形式均会对几何非线性计算结果产生影响,在大变形工程计算中需要考虑几何非线性,以获得足够的计算精度。A test and theoretical analysis were conducted for the reinforced wall panel of composite material, the calculation result is in accordance with the test well; the comparative analysis on linearity and geometrical non-linearity was done on the basis, the result shows the geometrical non-linearity can improve rigidity and strength of reinforced wall panel. With comparison of linearity and geometrical non-linearity calculation results, it is known that the structural rigidity and form can affect geometrical non-linearity calculation result, so it needs to consider the geometrical non-linearity in the calculation of big deformation project to obtain sufficient calculation accuracy.
分 类 号:V214.8[航空宇航科学与技术—航空宇航推进理论与工程]
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