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Curvilinear Fatigue Crack Growth Simulation and Validation under Constant Amplitude and Overload Loadings
- Source :
- Journal of Aerospace Engineering. 28
- Publication Year :
- 2015
- Publisher :
- American Society of Civil Engineers (ASCE), 2015.
-
Abstract
- A concurrent simulation and experimental validation for curvilinear fatigue crack growth (FCG) analysis under both constant amplitude and overload spectrums is proposed in this paper. The simulation methodology is based on a small time-scale fatigue crack growth model and the extended finite element method (XFEM) to calculate the stress intensity factor solution of an arbitrary curvilinear crack. Parametric studies are used to determine the algorithm parameters in the numerical fatigue crack growth simulation. Following this, experimental testing on modified compact specimens is performed under both constant amplitude and overload loadings for model validation. Experimentally measured crack growth orientations and lengths are compared with numerical simulations. Both the experimental and simulation results show the overload retardation behavior for curvilinear cracks under overload loadings. The investigated periodic overload loading has no significant impact on the crack growth orientations. Seve...
- Subjects :
- Curvilinear coordinates
Materials science
business.industry
Mechanical Engineering
Aerospace Engineering
Structural engineering
Paris' law
Physics::Classical Physics
Crack closure
Amplitude
General Materials Science
Constant (mathematics)
business
Stress intensity factor
Civil and Structural Engineering
Extended finite element method
Parametric statistics
Subjects
Details
- ISSN :
- 19435525 and 08931321
- Volume :
- 28
- Database :
- OpenAIRE
- Journal :
- Journal of Aerospace Engineering
- Accession number :
- edsair.doi...........42eeddf9e1f1c5edd994941b2631ca71