摘要
本文讨论了基于二次规划理论的三维弹塑性接触问题,其数值解法采用极大极小对偶迭代法,此方法比较简单、容易编制程序并且有严格的算法收敛性证明,方法适用于各种类型结构的接触问题。最后给出某型号飞机的机身与起落架之间的轴-套简结构的计算实例。
This paper discusses a solution method for three dimensional elastic-plastic contact problems based on the guadratic programming theory. The numerical methecl. a max-min dual iterative method, is simple and very easy in programming. The convergence of the algorithm has been proved. Finally, we give a numerical example which is an axle-tube structure connecting the fuselage and landing gear of an aircraft. The numerical results show that the method is efficient.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1990年第3期A140-A145,共6页
Acta Aeronautica et Astronautica Sinica
关键词
弹塑性
接触
二次规划
飞机
三维
elastic-plastic contact, quadratic program, max-min dual iteration.