METHOD FOR FATIGUE LIFE ANALYSIS OF SHEAR JOINT FASTENERS IN METAL–COMPOSIT JOINTS OF Aircraft Structural ELEMENTS
Abstract
By results of the review, the analysis and use of data of activities [1-8] substantive provisions of a method for fatigue life analysis of shear joint fasteners in metal-composit joints of aircraft structural elements are formulated and presented. It is noticed, that a main objective of working out and application of the presented method – search of the erroneous is constructive-technological decisions yielding unsatisfactory settlement and experimental results on fatigue durability of shear joints in mixed packages.
References
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Review
For citations:
Strizhius V.E. METHOD FOR FATIGUE LIFE ANALYSIS OF SHEAR JOINT FASTENERS IN METAL–COMPOSIT JOINTS OF Aircraft Structural ELEMENTS. Civil Aviation High Technologies. 2014;(199):52-61. (In Russ.)
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