Abstract
We present a methodology aimed at guaranteeing high fatigue and crack-growth resistance of aircraft structures in Russia and formulate criteria of survivability of these structures and requirements to the materials intended for the use in designed structures. We also analyze the methods used for the solution of the problem of safe operation of old aircrafts which take into account the degradation of fatigue and crack-growth resistance of structural materials and suggest a solution of the problem of multiple-origin cracks for aircraft structures in Russia.
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