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  • 英語翻譯

    英語翻譯
    Having the stiffness matrix for the adhesive as shown in equation (19),we can couple the stiffness matrix of the adhesive to the stiffness matrices of the composite patch and damaged laminate.According to Jones and Callinan [9],the interlaminar shear stresses τzx and τzy in the patch and laminate can be neglected with only a few percent error.In this investigation,the stiffness matrices of the composite patch and damaged laminate are derived based on the standard plane stress formulation.Using the standard finite element assembly procedure,we can incorporate the stiffness matrix of the adhesive along with the stiffness matrices of the composite patch and damaged laminate,thus producing the system stiffness matrix for the adhesively
    bonded composite laminate.
    英語人氣:740 ℃時間:2020-03-08 22:39:12
    優(yōu)質(zhì)解答
    有了方程(19)所示的膠粘劑剛度矩陣,我們就可以將膠粘劑的剛度矩陣與復(fù)合材料補片和損壞的層壓材料的剛度矩陣結(jié)合起來.根據(jù)瓊斯和卡里南的(理論或計算等)[9],層間剪切應(yīng)力τZX和補片與層壓材料的τZY可以忽略不計,其誤差只有百分之幾.本次科研中,在標(biāo)準(zhǔn)平面應(yīng)力公式的基礎(chǔ)上推導(dǎo)出了復(fù)合材料補片和損壞的層壓材料的剛度矩陣.通過使用標(biāo)準(zhǔn)的有限元裝配程序,我們可以將膠粘劑的剛度矩陣與復(fù)合材料補片和損傷層壓板的剛度矩陣合并,從而產(chǎn)生粘結(jié)復(fù)合材料的系統(tǒng)剛度矩陣.
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