Evaluation of fatigue damage using nonlinear guided waves
By Christoph Pruell, Jin-Yeon Kim, Jianmin Qu, Laurence J. Jacobs. 2009
220 citations recorded by the source corpus.
Subfields: Mechanical Engineering, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/38a5eb21e54668507622fba4ef3ad3cf9b30bdf2
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Mechanical Engineering
- Srinivasan Gopalakrishnan
- M. Mitra
- Jin-Yeon Kim
- J. M. Vivar-Perez
- Laurence J. Jacobs
- Jianmin Qu
- Z. Ahmad
- C. Willberg
In Mechanics of Materials
- Jin-Yeon Kim
- Laurence J. Jacobs
- Jianmin Qu
- Srinivasan Gopalakrishnan
- M. Mitra
- K. Matlack
- J. M. Vivar-Perez
- Z. Ahmad
Citations in the corpus
- Ultrasonic waves for materials evaluation in fatigue, thermal and corrosion damage: A review (2019, unknown): “So, to obtain the value of the non-linear ultrasonic coefficient 𝛽 is necessary to measure the absolute amplitude of the ultrasonic wave 𝐴 1 and 𝐴 2 [45] [46] [47].”
- Review of Second Harmonic Generation Measurement Techniques for Material State Determination in Metals (2015, background): “uration at higher fatigue cycles was also seen with nonlinear Lamb waves in an Al-1100 alloy [84].”
- Fatigue damage evaluation in A36 steel using nonlinear Rayleigh surface waves (2012, result): “This behavior is consistent with experimental results in other materials with a variety of loading conditions [1–10], and adds additional credence to the conclusion that the measured acoustic nonlinearity is plasticity driven.”
- Simulation Methods for Guided Wave-Based Structural Health Monitoring: A Review (2015, background): “investigated the detection of plasticity and fatigue damage with Lamb waves [200, 201].”
- Guided wave based structural health monitoring: A review (2016, methodology): “The Lamb wavedispersion plot with response spectrogram indicating same wave velocities for fundamental and second harmonics [272] is presented in figure 10(a) and the corresponding frequency domain response is shown in figure 10(b) for a low cycle fatigue aluminum specimen.”