[an error occurred while processing this directive]
   
 
���¿��ټ��� �߼�����
   ��ҳ  �ڿ�����  ��ί��  Ͷ��ָ��  �ڿ�����  ��������  �� �� ��  ��ϵ����
�������պ����ѧѧ�� 2012, Vol. 38 Issue (6) :715-719    DOI:
���� ����Ŀ¼ | ����Ŀ¼ | ������� | �߼����� << | >>
������ϸ�ڽṹ�;�������������ͳ�Ʊ궨
��С��, ������, ����ë, ���ĬE*
�������պ����ѧ, ���տ�ѧ�빤��ѧԺ, ���� 100191
Statistical scaling of durability life for independent multi-detail structures
He Xiaofan, Dong Yanmin, Liu Yanmao, Liu Wenting*
School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

ժҪ
�����
�������
Download: PDF (375KB)   HTML 1KB   Export: BibTeX or EndNote (RIS)      Supporting Info
ժҪ �ڽ���ƣ�����������ṹ����ʱ,Ϊ������ʵģ��ʵ�ʽṹ��ʽ�ʹ������,ģ���Լ�������Ƴɶ�ϸ���Լ�,���в���ȫƣ����������,�����ɶ�ϸ���Լ������ƶϵ�ϸ������.��Թ����ϳ��õ����������ֲ���ʽ:������̬�ֲ���˫����Weibull�ֲ�,�Խṹ����ʧЧģ��Ϊ����,����������ͬ������ϸ�ڽṹƣ�������ֲ�ȷ����ϸ�������ֲ���ͳ�Ʊ궨����.����ϸ���Լ��������Ӷ�����̬�ֲ�ʱ,�ɽ�����Ϊ��ϸ������Ҳ���Ӷ�����̬�ֲ�,��ϸ�������ֲ��������ϸ���Լ������ֲ����������ȷ����ϵ,���ҵ�ϸ��������ѧ�����ͱ�׼������ڶ�ϸ���Լ���Ӧ����;����ϸ����������˫����Weibull�ֲ�ʱ,��ϸ������Ҳ����˫����Weibull�ֲ�,��б�ʲ���,��λ�ò����������Ŵ�.��������һ������ʵ��.
Service
�ѱ����Ƽ�������
�����ҵ����
�������ù�����
Email Alert
RSS
�����������
����
������
����ë
���ĬE
�ؼ����� ƣ��   ʹ������   ��ϸ��   ������̬�ֲ�   Weibull�ֲ�   ͳ�Ʊ궨     
Abstract�� To assess the fatigue life for aircraft structure, the specimen used for the durability test is often designed as multi-details(MD) to simulate the structural configuration and load transfer. Once one detail fails, the fatigue testing is ended, and the fatigue life of single detail(SD) must be deduced statistically based on the incomplete life of MD specimen. Based on the series failure model of the same multi-detail structures, the statistical scaling approach was proposed to determine the life distribution of the single detail. Assuming the fatigue life of MD follows the log-normal distribution, Monte Carlo sampling and stimulating results show that the fatigue life of single detail follows the same distribution approximately; the expressions between the distribution parameters of MD and SD are deduced. The expectation and variation of MD are higher than those of SD. Assuming the fatigue life of MD follows the two-parameter Weibull distribution, the SD��s fatigue life follows the same distribution whose slope is unchanged, but location parameter is larger than that of MD. Finally, an example for analyzing MD fatigue test result from American durability test program is given.
Keywords�� fatigue   service life   multi-details   log-normal   Weibull distribution   statistical scaling     
Received 2011-03-15;
Fund:������Ȼ��ѧ����������Ŀ(11002009)
���ñ���:   
��С��, ������, ����ë, ���ĬE.������ϸ�ڽṹ�;�������������ͳ�Ʊ궨[J]  �������պ����ѧѧ��, 2012,V38(6): 715-719
He Xiaofan, Dong Yanmin, Liu Yanmao, Liu Wenting.Statistical scaling of durability life for independent multi-detail structures[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2012,V38(6): 715-719
���ӱ���:  
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2012/V38/I6/715
Copyright 2010 by �������պ����ѧѧ��