Modeling of Crack Growth With Dwell Time for Aero-Engine Spectra Loadings in a Ni-Based Superalloy
Keyword(s):
Testing and simulation of aero-engine spectra with dwell times are reported in this paper. The modeling concept used is built on linear elastic fracture mechanics (LEFM) and provides a history-dependent evolution description of dwell damage and its interaction with cyclic load. The simulations have been carried out for three spectra: (1) cyclic loads, (2) combined sustained load and cyclic loads, and (3) slow load ramps and cyclic loads, all for surface cracks at 550 °C for Inconel 718. All simulations show reasonable good agreement with experimental results. Prediction of multiple tests of several batches is also provided to show statistical scatter.
Keyword(s):
2007 ◽
Vol 42
(5)
◽
pp. 361-375
◽
Keyword(s):
Keyword(s):
2017 ◽
Vol 730
◽
pp. 489-495
◽
Keyword(s):
2005 ◽
Vol 219
(1)
◽
pp. 1-10
◽