Fatigue crack propagation in AA 7050-T7451 alloy considering environment, stress ratio, rolling direction and waveform effects
Main extrinsic and intrinsic modifiers factors of crack growth rate in AA7050-T7451 were assessed in order to provide tools for aeronautical structures designers. These tools cover most necessary information to project aircraft\'s structures using the studied alloy, under damage tolerance philo...
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| Format: | Others |
| Language: | en |
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Biblioteca Digitais de Teses e Dissertações da USP
2017
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| Online Access: | http://www.teses.usp.br/teses/disponiveis/18/18158/tde-27062017-111140/ |