Residual strains surrounding split-sleeve cold expanded holes in 7075-T651 aluminum
LINK, R. E., SANFORD, R. J.
JOURNAL OF AIRCRAFT ; 27 , 7 ; 599-604
1990
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Aluminum Alloy Plate - 5.6zn - 2.5mg - 1.6cu - 0.26cr (7075-T651)
SAE Technical Papers | 1968
Split Sleeve Cold Expansion as a Rework Process for Previously Cold Expanded Holes
British Library Conference Proceedings | 1993
|Aluminum Alloy Plate, Alclad - 5.6zn - 2.5mg - 1.6cu - 0.26cr (Alclad 7075-T651)
SAE Technical Papers | 1968
SAE Technical Papers | 1965
INTERGRANULAR CORROSION PROTOCOL DEVELOPMENT FOR 7075-T651 EXTRUSION
British Library Conference Proceedings | 2012
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