ANALYSIS OF RESIDUAL STRESSES WHEN USING CONSTRUCTIVE AND TECHNOLOGICAL METHODS OF INCREASING FATIGUE LIFE. MESSAGE 1. FREE HOLE
Increasing the fatigue life of elements of aircraft structures by methods based on local plastic deformation of the material in the hole zone directly depends on the magnitude and sign of the residual stresses. This paper presents the results of the study of residual stresses, which are formed when...
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| Format: | Article |
| Language: | English |
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National Aerospace University «Kharkiv Aviation Institute»
2019-07-01
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| Series: | Авіаційно-космічна техніка та технологія |
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| Online Access: | http://nti.khai.edu/ojs/index.php/aktt/article/view/740 |