摘要
本文利用复变函数方法导出含孔边双侧直线裂纹有限大板应力与位移的全场表达式,满足所有基本方程式、裂纹表面边界条件与复连通域位移单值条件。应用变分原理满足其余边界条件并求解应力强度因子。变分方程中只有线积分。故本方法计算效率较高。
Total field expressions of stress and displacement components in a finite monolithic plate with double linear hole edge crack are derived by means of method of functions of complex variables, and all of the basic equations, boundary conditions of crack surfaces and single-valued condition of displacements about multi-connected region are satisfied exactly. The stress intensity factors are solved by means of variational method to satisfy the other boundary conditions. In the variational equations there are only line integrals and no area integrals. The convergency is very rapid and the method is time-saving. Then, systematical results are presented by curves of nondimensional stress intensity factor versus nondimensional crack lengths with nondimensional hole radii and aspect ratios as parameters. Finally, the analytical-variational method is extended to the case without cracks, the convergency is nice also and systematical results are provided by-curves of stress concentration factors versus nondimensional hole radii with aspect ratios as parameters.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1992年第11期A602-A609,共8页
Acta Aeronautica et Astronautica Sinica
关键词
孔边裂纹
变分法
裂纹
飞机
Hole-edge crack, Recurrence formula of displacement, Single-valued condition of displacement, Variational method