Determination of the viscosity factor of D16 aluminum alloy in penetration of a cone

1984 ◽  
Vol 16 (10) ◽  
pp. 1484-1489 ◽  
Author(s):  
G. V. Stepanov ◽  
A. P. Vashchenko
2011 ◽  
Vol 291-294 ◽  
pp. 1039-1042
Author(s):  
Wei Xie ◽  
Shao Wei Tu ◽  
Qi Qing Huang ◽  
Ya Zhi Li

In the present work, the resistance to crack extension of 2524-T3 aluminum alloy under Mode I loading was studied by using the middle-cracked tension M (T) specimens. The curve, plane-stress fracture toughness and apparent plane-stress fracture toughness were calculated by test data. The average value of measured fracture toughness at room temperature was 161 MPam1/2. The results and conclusions can be referred in airplane skin design.


1962 ◽  
Vol 11 (1) ◽  
pp. 43-47 ◽  
Author(s):  
Masaru ISHIBASHI ◽  
Hitoshi KOMAKI

Talanta ◽  
2009 ◽  
Vol 79 (4) ◽  
pp. 1001-1005 ◽  
Author(s):  
Tsuyoshi Kagawa ◽  
Masashi Ohno ◽  
Tatsuya Seki ◽  
Katsumi Chikama

2013 ◽  
Vol 337-338 ◽  
pp. 1-4
Author(s):  
N.A. Kamel ◽  
S.A. Aly ◽  
A.A. Ibrahim ◽  
E.A. Badawi

Electrical techniques have been used to study the thermal vacancies in 401.0 casting aluminum alloy. Quenching experiments were usually performed on thin specimens to ensure a uniform quenching rate throughout the specimen. After grinding, polishing and etching, samples of 401.0 were homogenized for 12h at 673K and annealed for 90min., before quenched in water (277K) and then subjected to electrical measurements. From such measurements it is possible to deduce the vacancy formation enthalpy, which in combination with the results of self-diffusion measurements, give a value for the migration enthalpy of the vacancy.


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