Научный вестник МГТУ ГА (Jan 2017)
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.