Titlebook: Riveted Lap Joints in Aircraft Fuselage; Design, Analysis and Andrzej Skorupa,Malgorzata Skorupa Book 2012 Springer Science+Business Media

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Predictions of Fatigue Crack Growth and Fatigue Life for Riveted Lap Joints,). It is well known that due to the anomalous behaviour of small cracks such predictions can be unreliable and lead to unconservative results in the early stage of crack growth from the initial defect. A concept of the equivalent initial flaw size (EIFS) developed by Rudd and Gray (1976, 1978) and M

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Book 2012sign solutions and loading conditions for fuselage skin joints; relevance of laboratory test results for simple lap joint specimens to riveted joints in a real structure; effect of various production and design related variables on the riveted joint fatigue behaviour; analytical and experimental res

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Decibel

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EWER

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