ASD-STAN PREN 2318-1980 Aluminium Alloy 2024-T3510 or T3511 - Bars and Sections 1 2 mm Less Than or Equal to a Less Than or Equal to 150 mm Aerospace Series (Edition 1)《航空航天系列 铝合金2.pdf

《ASD-STAN PREN 2318-1980 Aluminium Alloy 2024-T3510 or T3511 - Bars and Sections 1 2 mm Less Than or Equal to a Less Than or Equal to 150 mm Aerospace Series (Edition 1)《航空航天系列 铝合金2.pdf》由会员分享，可在线阅读，更多相关《ASD-STAN PREN 2318-1980 Aluminium Alloy 2024-T3510 or T3511 - Bars and Sections 1 2 mm Less Than or Equal to a Less Than or Equal to 150 mm Aerospace Series (Edition 1)《航空航天系列 铝合金2.pdf（3页珍藏版）》请在麦多课文档分享上搜索。

AECMA PRENZLB 80 -m 1r012311 ooo2_ew 7 m - - - - I A.E.C.M.A. STANDARD DRAFT Edition 1 October 1980 NORME A.E.G.M.A. A. E.C.M.A. NORM pr E N 231 8 ENGLISH VERSION ALUMINIUM ALLOY 2024-T35 or T35fl BARS AND SECTIONS 1,s mm 10 Wo 460 , 460 2 480 12 4 a 11 5) 2. 10 10 - I I 1 1 - - - -. I- I I I -I Hardness I 120 (for information) - Shear Strength Bendlng Im e I Ruptura ElonQetlon nt ruptum A Notor AECMA PREN2318 AO W L01231l 0002874 O W 1 , r!. *.: 1 Electrical conductivity I, 1. . -. , dotan rypical use 2 3 4 5 6 7 17 100 mm r I