2000
DOI: 10.1006/jsvi.2000.2981
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Non-Linear Vibration Method for Detection of Fatigue Cracks in Aircraft Wings

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Cited by 81 publications
(34 citation statements)
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“…They noted some nonlinear features of the spectra; they in fact observed a modest crack signature from a crack halfway through the thickness of a simply supported beam. More recently, researchers have been looking at the steady state response of the beam to a single harmonic input while including the non linear effects of crack closure and outlining procedures of sub-and super-resonant diagnostics [7].…”
Section: Introductionmentioning
confidence: 99%
“…They noted some nonlinear features of the spectra; they in fact observed a modest crack signature from a crack halfway through the thickness of a simply supported beam. More recently, researchers have been looking at the steady state response of the beam to a single harmonic input while including the non linear effects of crack closure and outlining procedures of sub-and super-resonant diagnostics [7].…”
Section: Introductionmentioning
confidence: 99%
“…They also observed antiresonance frequency shifts and super/subharmonic vibration phenomena in the experimental study of naturally grown fatigue cracks. It was also observed in the bending vibration encountered in an aircraft wing under external harmonic excitation [18] that elastic nonlinearity of crack results in the generation of superharmonic vibration regimes. In [19], nonlinear systems of algebraic equations were defined to model the cantilever beam with several breathing cracks to study the vibration response.…”
Section: Introductionmentioning
confidence: 86%
“…3). Some adjustment occurs due to the nonlinear dependence À 2 on the ratio of the parameter a d [see formulas (13)]. …”
mentioning
confidence: 99%
“…For the considered case of excitation of vibrations of a hinge-supported rod, the difference between the data calculation by formulas (27) and (29) . for x l c = 0.1, 0.25, and 0.5, their corresponding values of the nonlinearity parameter of the vibration process À 2 for the vibration decrement d = 0.01 were calculated using formulas (27) and (29), (30) and relationships (13). For convenience of the further analysis, the dependences of the relative acceleration amplitude of the second harmonic À à 2 on the point of application of the driving force for the cases of different locations of the crack x l c are presented in Fig.…”
mentioning
confidence: 99%
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