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 in | International journal of fatigue Vol. 45; pp. 82 - 90 |
|---|---|
| Main Authors | , |
| Format | Journal Article |
| Language | English |
| Published |
Kidlington
Elsevier Ltd
01.12.2012
Elsevier |
| Subjects | |
| Online Access | Get full text |
| ISSN | 0142-1123 1879-3452 |
| DOI | 10.1016/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 |
| Author_xml | – sequence: 1 givenname: Mark surname: Paulus fullname: Paulus, Mark email: mark.paulus@navy.mil organization: Advanced Test Development, Naval Undersea Warfare Center Division Keyport, 610 Dowell St., Keyport, WA 98345, USA – sequence: 2 givenname: Abhijit surname: Dasgupta fullname: Dasgupta, Abhijit email: dasgupta@umd.edu organization: Center for Advanced Life Cycle Engineering (CALCE), 2110C Glenn L. Martin Hall, Building 088, University of Maryland, College Park, MD 20742, USA |
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| Cites_doi | 10.1115/1.3667396 10.1016/j.ndteint.2004.05.004 10.17764/jiet.53.1.167m8136u6514056 10.1111/j.1747-1567.2006.00083.x 10.17764/jiet.44.4.f72822w825r1156j 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 |
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| References | Paulus, Dasgupta, Habtour (b0045) 2011 French, Handy, Cooper (b0030) 2006; 30 He, Fu (b0075) 2001 Paulus, Doughty (b0040) 2010; 53 Ungar (b0060) 1962; 84 Habtour, Choi, Osterman, Dasgupta (b0020) 2012 Steinberg (b0015) 2001 Paulus (b0025) 2011; 54 Douka, Hadjileontiadis (b0065) 2005; 38 Modarres, Kaminskiy, Krivtsov (b0085) 2010 Nelson (b0090) 2004 Irvine (b0055) 1999 Fackler, Warren (b0005) 1972 Whiteman (b0035) 2001; 44 Montgomery (b0080) 1997 Stephens, Fatemi, Stephens, Fuchs (b0050) 2001 Balachandran, Magrab (b0070) 2009 MIL-STD-810G. “Environmental engineering considerations and laboratory tests”. Irvine (10.1016/j.ijfatigue.2012.06.008_b0055) 1999 10.1016/j.ijfatigue.2012.06.008_b0010 Modarres (10.1016/j.ijfatigue.2012.06.008_b0085) 2010 Whiteman (10.1016/j.ijfatigue.2012.06.008_b0035) 2001; 44 Habtour (10.1016/j.ijfatigue.2012.06.008_b0020) 2012 Paulus (10.1016/j.ijfatigue.2012.06.008_b0040) 2010; 53 Balachandran (10.1016/j.ijfatigue.2012.06.008_b0070) 2009 Montgomery (10.1016/j.ijfatigue.2012.06.008_b0080) 1997 French (10.1016/j.ijfatigue.2012.06.008_b0030) 2006; 30 Stephens (10.1016/j.ijfatigue.2012.06.008_b0050) 2001 He (10.1016/j.ijfatigue.2012.06.008_b0075) 2001 Nelson (10.1016/j.ijfatigue.2012.06.008_b0090) 2004 Paulus (10.1016/j.ijfatigue.2012.06.008_b0045) 2011 Ungar (10.1016/j.ijfatigue.2012.06.008_b0060) 1962; 84 Steinberg (10.1016/j.ijfatigue.2012.06.008_b0015) 2001 Douka (10.1016/j.ijfatigue.2012.06.008_b0065) 2005; 38 Fackler (10.1016/j.ijfatigue.2012.06.008_b0005) 1972 Paulus (10.1016/j.ijfatigue.2012.06.008_b0025) 2011; 54 |
| References_xml | – volume: 53 year: 2010 ident: b0040 article-title: Effect of resonant frequency shifting on time to failure of a cantilevered beam under vibration publication-title: J IEST – year: 2011 ident: b0045 article-title: Life estimation model of a cantilevered beam subjected to random vibration publication-title: Fatigue Fract Eng Mater – year: 2001 ident: b0075 article-title: Modal analysis – volume: 30 start-page: 32 year: 2006 end-page: 37 ident: b0030 article-title: Comparison of simultaneous and sequential single axis durability testing publication-title: Experiment Tech – year: 1999 ident: b0055 article-title: Optimal use of the vibration response spectrum for enveloping random data publication-title: Proc Inst Environ Sci Technol – volume: 38 start-page: 3 year: 2005 end-page: 10 ident: b0065 article-title: Time-frequency analysis of the free vibration response of a beam with a breathing crack publication-title: NDT&E Int – year: 2004 ident: b0090 article-title: Accelerated testing: statistical models, test plans, and data analysis – year: 1972 ident: b0005 article-title: Equivalence techniques for vibration testing – year: 2001 ident: b0015 article-title: Preventing thermal cycling and vibration failures in electronic equipment – year: 2012 ident: b0020 article-title: Novel approach to improve electronics reliability in the next generation of US army small unmanned ground vehicles under complex vibration conditions publication-title: J Fail Anal Prevent – year: 1997 ident: b0080 article-title: Design and analysis of experiments – reference: MIL-STD-810G. “Environmental engineering considerations and laboratory tests”. – volume: 54 year: 2011 ident: b0025 article-title: Limitations of the power spectral density as an indicator of test severity publication-title: J IEST – year: 2010 ident: b0085 article-title: Reliability engineering and risk analysis – year: 2001 ident: b0050 article-title: Metal fatigue in engineering – volume: 44 start-page: 20 year: 2001 end-page: 23 ident: b0035 article-title: Inadequacies in uniaxial stress screen vibration testing publication-title: J IEST – volume: 84 start-page: 149 year: 1962 end-page: 155 ident: b0060 article-title: Maximum stresses in beams and plates vibrating at resonance publication-title: J Eng Ind – year: 2009 ident: b0070 article-title: Vibrations – year: 1999 ident: 10.1016/j.ijfatigue.2012.06.008_b0055 article-title: Optimal use of the vibration response spectrum for enveloping random data publication-title: Proc Inst Environ Sci Technol – volume: 84 start-page: 149 year: 1962 ident: 10.1016/j.ijfatigue.2012.06.008_b0060 article-title: Maximum stresses in beams and plates vibrating at resonance publication-title: J Eng Ind doi: 10.1115/1.3667396 – year: 2001 ident: 10.1016/j.ijfatigue.2012.06.008_b0015 – volume: 38 start-page: 3 year: 2005 ident: 10.1016/j.ijfatigue.2012.06.008_b0065 article-title: Time-frequency analysis of the free vibration response of a beam with a breathing crack publication-title: NDT&E Int doi: 10.1016/j.ndteint.2004.05.004 – volume: 53 issue: 1 year: 2010 ident: 10.1016/j.ijfatigue.2012.06.008_b0040 article-title: Effect of resonant frequency shifting on time to failure of a cantilevered beam under vibration publication-title: J IEST doi: 10.17764/jiet.53.1.167m8136u6514056 – year: 2011 ident: 10.1016/j.ijfatigue.2012.06.008_b0045 article-title: Life estimation model of a cantilevered beam subjected to random vibration publication-title: Fatigue Fract Eng Mater – volume: 30 start-page: 32 year: 2006 ident: 10.1016/j.ijfatigue.2012.06.008_b0030 article-title: Comparison of simultaneous and sequential single axis durability testing publication-title: Experiment Tech doi: 10.1111/j.1747-1567.2006.00083.x – year: 2009 ident: 10.1016/j.ijfatigue.2012.06.008_b0070 – year: 2001 ident: 10.1016/j.ijfatigue.2012.06.008_b0075 – year: 1972 ident: 10.1016/j.ijfatigue.2012.06.008_b0005 – year: 2001 ident: 10.1016/j.ijfatigue.2012.06.008_b0050 – volume: 44 start-page: 20 year: 2001 ident: 10.1016/j.ijfatigue.2012.06.008_b0035 article-title: Inadequacies in uniaxial stress screen vibration testing publication-title: J IEST doi: 10.17764/jiet.44.4.f72822w825r1156j – year: 2010 ident: 10.1016/j.ijfatigue.2012.06.008_b0085 – volume: 54 issue: 2 year: 2011 ident: 10.1016/j.ijfatigue.2012.06.008_b0025 article-title: Limitations of the power spectral density as an indicator of test severity publication-title: J IEST doi: 10.17764/jiet.54.2.j3761476322338w1 – year: 1997 ident: 10.1016/j.ijfatigue.2012.06.008_b0080 – ident: 10.1016/j.ijfatigue.2012.06.008_b0010 – year: 2004 ident: 10.1016/j.ijfatigue.2012.06.008_b0090 – year: 2012 ident: 10.1016/j.ijfatigue.2012.06.008_b0020 article-title: Novel approach to improve electronics reliability in the next generation of US army small unmanned ground vehicles under complex vibration conditions publication-title: J Fail Anal Prevent doi: 10.1007/s11668-011-9533-1 |
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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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