The Simulation of the Fatigue Fracture Process at Random Loading
2013 ◽
Vol 592-593
◽
pp. 113-116
Keyword(s):
The general scheme of crack growth modeling and periodicity of aviation structure elements checks was developed. The major factors determined the scale of inaccuracy calculation ( εN*) based on calculations of crack growth duration (N*) and inspections intervals (τ0) were marked and estimated with the block diagram.
Keyword(s):
2020 ◽
Vol 185-186
◽
pp. 65-77
◽
Keyword(s):
2020 ◽
Vol 107
◽
pp. 102529
◽
2014 ◽
Vol 58
◽
pp. 66-74
◽
Keyword(s):
2015 ◽
Vol 138
(1)
◽
2013 ◽
Vol 33
◽
pp. 126-134
◽
2013 ◽
Vol 10
(2)
◽
pp. 46
Keyword(s):