卷边加筋肋约束下正交各向异性板剪切屈曲荷载的近似公式OA
Approximate formulas of shear buckling load of orthotropic plates restrained by lipped stiffeners
构造恰当的屈曲形函数,采用瑞利-里兹法求解两对边简支、另外两对边受卷边加筋肋约束的正交各向异性板临界剪切屈曲荷载的解析解.引入无量纲正交各向异性参数、翘曲约束系数和两类屈曲系数,利用曲线拟合技术得到卷边加筋肋约束下正交各向异性板临界剪切屈曲荷载的近似计算公式.将得到的近似公式与解析解、转换解和ANSYS数值解进行对比,验证近似公式的有效性和通用性.求解得到的近似公式可以应用到具有卷边翼缘的复合材料型材的剪切局部屈曲分析中.
The analytical solution for in-plane shear-loaded orthotropic plates,where two opposite edges are simply supported and the other two are restrained by lipped stiffeners with warping stiffness,is obtained using the Rayleigh-Ritz method and a proper buckled shape function.By introducing generic non-dimensional parameters,i.e.,orthotro-pic material parameters,warping constraint coefficient,and two types of buckling coefficients,the approximate formu-las of the critical shear buckling load of orthotropic plates restrained by lipped stiffeners with warping stiffness are ob-tained by using the curve-fitting technique.The effectiveness and generality of the approximate formulas are validated with the analytical and transformed solutions,and ANSYS numerical analysis.The obtained approximate formulas can be applied to the local buckling analysis of composite beams with edge-stiffened flanges subjected to shear loads.
丁慧;刘庆辉;乔丕忠
河海大学 力学与工程科学学院,南京 211100河海大学 力学与工程科学学院,南京 211100上海交通大学 船舶海洋与建筑工程学院,上海 200240
通用工业技术
正交各向异性板临界屈曲荷载瑞利-里兹法卷边加筋肋均匀剪切复合材料
orthotropic platescritical buckling loadRayleigh-Ritz methodlipped stiffenersuniform shearcomposites
《复合材料科学与工程》 2026 (4)
36-43,8
国家自然科学基金(52279129)
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