THE FATIGUE CRACK GROWTH BEHAVIOR OF THE Al?Cu?Li ALLOY WELDALITE 049-Reference-Cited by-同舟云学术

THE FATIGUE CRACK GROWTH BEHAVIOR OF THE Al?Cu?Li ALLOY WELDALITE 049

Published:1991-01 Issue:1 Volume:14 Page:103-114
ISSN:8756-758X
Container-title:Fatigue & Fracture of Engineering Materials and Structures
language:en
Short-container-title:Fat Frac Eng Mat Struct

Author:

Blankenship C. P.,Starke E. A.

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/j.1460-2695.1991.tb00646.x/fullpdf

Reference26 articles.

1. 1. J. R. Pickens, F. H. Heubaum, T. J. Langan, L. S. Kramer, T. H. Sanders, and E. A. Starke (1989 ) Al-(4.5-6.3) Cu-1.3 Li-0.4 Ag-0.4 Mg-0.14 Zr Alloy Weldalite(tm) 049. Aluminum-Lithium Alloys V (Edited by), Vol. III , pp.1397 -1414 . MCE, Birmingham, England.

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