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van der Linden, H.H. (author), de Koning, A.U. (author), Lof, C.J. (author)After a discussion of some aspects of aircraft design philosophy and the fatigue phenomenon, two analytical techniques for prediction of crack growth rates are described. The first method includes a model for prediction of fatigue crack growth in aluminium alloy sheet specimens subjected to service loading conditions. The second method involves...report 1982