Pages that link to "Item:Q2882018"
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The following pages link to Non-linear vibration method for detection of fatigue cracks in aircraft wings (Q2882018):
Displaying 9 items.
- Location identification of nonlinearities in MDOF systems through order determination of state-space models (Q333067) (← links)
- A nonlinear decomposition and regulation method for nonlinearity characterization (Q335476) (← links)
- Detection and description of non-linear phenomena in experimental modal analysis via linearity plots (Q873451) (← links)
- A novel damage detection approach by using Volterra kernel functions based analysis (Q1660543) (← links)
- A new nonlinear elastic time reversal acoustic method for the identification and localisation of stress corrosion cracking in welded plate-like structures - A simulation study (Q2382468) (← links)
- Vibroacoustic method of free oscillations for nondestructive crack testing (Q2719379) (← links)
- Global crack detection using bispectral analysis (Q3503325) (← links)
- In-Flight Vibration Monitoring of Aeronautical Structures (Q5375633) (← links)
- Primary and secondary resonances in pipes conveying fluid with the fractional viscoelastic model (Q6186745) (← links)