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,he residual strength of a structure is insufficient to sustain the prevailing loads, and rapid failure occurs. Aircraft manufacturers were the first industrial branch to place reliance on damage tolerance designs. It was assumed that initial imperfections and flaws inherent in the material or introd

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Residual Strength Predictions for Riveted Lap Joints in Fuselage Structures,derable amount of stable tearing followed by fast final failure. The term residual strength corresponds to the applied load level at which unstable crack growth occurs. As already said in Chap. 8, the increasing usage of aging aircraft triggered the attention to the problem of MSD. A host of experim

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Secondary Bending for Mechanically Fastened Joints with Eccentricities,duced along the faying surface at location A of sheet 1 and location B of sheet 2. Because outside the outer rivet rows either sheet carries the full applied tensile load, A and B are also locations of the maximum combined tensile stresses and, therefore, the most commonly observed fatigue crack initiation sites.

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Kenneth S. Thomas,Harold J. McMannvalue in framing fruitful questions for psychologists and others to pose and fruitful activities for psychologists and others to undertake. I use the term to identify what Rappaport (1987) called the phenomena of interest, i.e., “the entire class of phenomena that we want our research to undertake,

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