Semi-empirical life model of a cantilevered beam subject to random vibration

► Natural frequency change must be accounted for during random vibration. ► Natural frequency change is used to model damage accumulation. ► Life estimation can be performed using the damage accumulation rate. ► Modeling accuracy is improved by account for natural frequency change. Life estimation o...

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Published inInternational journal of fatigue Vol. 45; pp. 82 - 90
Main Authors Paulus, Mark, Dasgupta, Abhijit
Format Journal Article
LanguageEnglish
Published Kidlington Elsevier Ltd 01.12.2012
Elsevier
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Online AccessGet full text
ISSN0142-1123
1879-3452
DOI10.1016/j.ijfatigue.2012.06.008

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Abstract ► Natural frequency change must be accounted for during random vibration. ► Natural frequency change is used to model damage accumulation. ► Life estimation can be performed using the damage accumulation rate. ► Modeling accuracy is improved by account for natural frequency change. Life estimation of structures subjected to non-uniform random vibration analysis has historically been done through the use of fatigue properties. In general, evaluation of the severity of the vibration environment is performed at the initial natural frequency. It is widely known, however, that many structures will undergo a frequency change during failure. If the random vibration is non-uniform with large peaks and valleys, the frequency change will result in a changing stress state that must be accounted for. Evaluation of the accumulated damage can be done through accounting for the natural frequency change. This model uses experimental data to determine two empirical constants to predict time to failure for various complex random vibration profiles. Although the new model will utilize an experimental component in lieu of FEA, the physics of the underlying failure will be retained. Additionally the model has shown good correlation to experimental data, and improvements over existing techniques.
AbstractList ► Natural frequency change must be accounted for during random vibration. ► Natural frequency change is used to model damage accumulation. ► Life estimation can be performed using the damage accumulation rate. ► Modeling accuracy is improved by account for natural frequency change. Life estimation of structures subjected to non-uniform random vibration analysis has historically been done through the use of fatigue properties. In general, evaluation of the severity of the vibration environment is performed at the initial natural frequency. It is widely known, however, that many structures will undergo a frequency change during failure. If the random vibration is non-uniform with large peaks and valleys, the frequency change will result in a changing stress state that must be accounted for. Evaluation of the accumulated damage can be done through accounting for the natural frequency change. This model uses experimental data to determine two empirical constants to predict time to failure for various complex random vibration profiles. Although the new model will utilize an experimental component in lieu of FEA, the physics of the underlying failure will be retained. Additionally the model has shown good correlation to experimental data, and improvements over existing techniques.
Life estimation of structures subjected to non-uniform random vibration analysis has historically been done through the use of fatigue properties. In general, evaluation of the severity of the vibration environment is performed at the initial natural frequency. It is widely known, however, that many structures will undergo a frequency change during failure. If the random vibration is non-uniform with large peaks and valleys, the frequency change will result in a changing stress state that must be accounted for. Evaluation of the accumulated damage can be done through accounting for the natural frequency change. This model uses experimental data to determine two empirical constants to predict time to failure for various complex random vibration profiles. Although the new model will utilize an experimental component in lieu of FEA, the physics of the underlying failure will be retained. Additionally the model has shown good correlation to experimental data, and improvements over existing techniques.
Author Dasgupta, Abhijit
Paulus, Mark
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10.1016/j.ndteint.2004.05.004
10.17764/jiet.53.1.167m8136u6514056
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10.17764/jiet.54.2.j3761476322338w1
10.1007/s11668-011-9533-1
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Keywords Fatigue
Frequency shift
Accelerated life
Random vibration
Life estimation
Vibration
Mechanical properties
Modeling
Language English
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Snippet ► Natural frequency change must be accounted for during random vibration. ► Natural frequency change is used to model damage accumulation. ► Life estimation...
Life estimation of structures subjected to non-uniform random vibration analysis has historically been done through the use of fatigue properties. In general,...
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SubjectTerms Accelerated life
Accounting
Applied sciences
Cantilever beams
Constants
Exact sciences and technology
Fatigue
Fatigue (materials)
Fatigue failure
Frequency shift
Life estimation
Mathematical models
Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology
Metals. Metallurgy
Random vibration
Resonant frequency
Title Semi-empirical life model of a cantilevered beam subject to random vibration
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