Experimental and numerical study of fatigue crack growth of aluminum alloy 2024-T3 single lap simple bolted and hybrid (adhesive/bolted) joints
Author:
Publisher
Elsevier BV
Subject
General Engineering,General Materials Science
Reference35 articles.
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4. Temperature effects on material behavior of aerospace aluminum alloys for subsonic and supersonic aircraft;Huda;J. Aerosp. Eng.,2010
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