Determination of Fracture Toughness and K-R Curve for 2524-T3 Aluminum Alloy
2011 ◽
Vol 291-294
◽
pp. 1039-1042
Keyword(s):
Mode I
◽
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.
1973 ◽
pp. 334-349
◽
Keyword(s):
1994 ◽
Vol 04
(C8)
◽
pp. C8-747-C8-752
◽
2018 ◽
Vol 140
(10)
◽
2005 ◽
Vol 44
(3)
◽
pp. 363-379
◽
Keyword(s):