DocumentCode :
2157517
Title :
Method of comparative estimation of materials fatigue damage
Author :
Stepanov, Vladimir M.
Author_Institution :
Novosibirsk State Tech. Univ., Russia
fYear :
2002
fDate :
2002
Firstpage :
47
Lastpage :
49
Abstract :
In order to improve the quality of estimates that are obtained from experiments with different loading cycles, we suggest the following method of materials fatigue testing. During rotation the sample is loaded with cylindrical bend. Cross-section of a sample represents a symmetric cross. Irregular rotation of a the sample within one turn creates different forms of loading cycle in relatively perpendicular sample walls. The sample has two stress concentration profiles. Therefore, in the first four points the loading pattern is different from the loading pattern form in the four points. This allows us to obtain more information and thus, get a better estimate of the influence of the load parameters on fatigue age of the sample.
Keywords :
aircraft; bending; fatigue testing; aircraft design; cylindrical bend loading; fatigue damage; fatigue resistance; loading cycle; loading pattern; materials fatigue testing; perpendicular sample walls; stress concentration; supportive details; Aerospace materials; Aerospace testing; Aircraft manufacture; Costs; Fatigue; Life estimation; Materials testing; Shafts; Stress; Surface cracks;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Science and Technology, 2002. KORUS-2002. Proceedings. The 6th Russian-Korean International Symposium on
Print_ISBN :
0-7803-7427-4
Type :
conf
DOI :
10.1109/KORUS.2002.1027955
Filename :
1027955
Link To Document :
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