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transient response of mechanical structures using modal analysis techniques. angela burgess PDF

301 Pages·1998·5.28 MB·English
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Preview transient response of mechanical structures using modal analysis techniques. angela burgess

imperial College of Science and Technology (University of London) TRANSIENT RESPONSE OF MECHANICAL STRUCTURES USING MODAL ANALYSIS TECHNIQUES. BY ANGELA BURGESS A thesis submitted in partial fulfilment for the degree of Doctor of Philosophy, and for the Diploma of Imperial College. Department of Mechanical Engineering, Research at a public imperial College, London SW7. research establishment. J a n u a r y 1 9 8 8. ARE(Portland) c ABSTRACT The use of experimental modal analysis techniques together with Fourier transform methods is considered for their application to the transient response analysis of structures. The limitations and validity of this approach are examined for linear structures, and a relationship derived that describes the errors involved due to time aliasing within the inverse discrete Fourier transform. The method is demonstrated with a simple beam using several experimental modal analysis procedures. The applicability of the same analysis and prediction techniques to non-linear structures is explored. The use of constant-force stepped-sine excitation and subsequent circle-fit modal analysis procedures for identifying non-linearities is reviewed. Also, the reciprocal-of-receptance analysis is extended for classifying and quantifying the non-linearity present. Results from non-linear systems subjected to impulse excitation are examined using various analyses. It is found that clear trends are evident.for different non-linearities, but they do not correspond to those from a constant-force stepped-sine test. Techniques for predicting the transient response for non-linear systems using data from experimental tests are examined, with the result that several different approaches are recommended depending on the non-linearity, the initial conditions and the type and accuracy required of the results. These prediction methods include using a specific linear model and developing non-linear models that accurately describe the transient response. Multi-degree-of-freedom systems with one non-linear element are also examined, as in many practical structures the non-linearity tends to be concentrated in a single component. The trends exhibited in the individual non-linear elements subjected to experimental modal analysis are found to correspond to those trends found in the resonances of the multi-degree-of-freedom systems. Similarly, the recommended techniques for transient response prediction of a non-linear structure correspond to those for non-linear elements under the same conditions. 2 ., CONTENTS Page Abstract. 2 List of tables. 8 List of figures. 10 Acknowledgements. 16 1 INTRODUCTION. 17 1.1 Badground and overview. 18 1.2 Objectives. 18 1.3 Contents of the thesis. 2 A REVIEW OF TRANSIENT RESPONSE ANALYSIS METHODS. 21 2.0 Introduction. 2.1 Time domain methods. 22 2.1 .l Numerical methods. 22 2.1.2 Duhamet’s integral. 23 2.1.3 Graphical methods. 25 2.2 Frequency domain methods. 26 2.2.1 Shock response spectra. 26 2.2.2 Fourier transform methods. 29 2.3 Discussion. 31 3 . . Page 3 A REVIEW OF FREQUENCY RESPONSE MElHODS FOR STRUCTURAL MODELLING. 3.0 Introduction. 32 3.1 Summary of essential modal theory. 33 3.2 Experimental testing for frequency response of structures. 37 3.3 Extracting modal properties from experimental frequency response data. 41 3.3.1 Single-degree-of-freedom (SDOF) analysis. 41 3.3.2 Multi-degree-of-freedom (MDOF) analysis. 43 3.3.3 Time domain analysis. 45 3.4 Application of frequency response data and modal parameters. 46 3.4.1 From modal model to spatial model. 46 3.4.2 Response prediction in the frequency domain. 47 3.4.3 Frequency response coupling for structural assemblies. 47 3.5 Discussion. 49 Figures for chapter 3. 50 4 REQUIREMENTS FOR TRANSIENT RESPONSE ANALYSIS USING FREQUENCY RESPONSE. 4.0 Introduction. 56 4.1 Fourier transform - from theory to practice. 58 4.2 Limitations of using the ‘Fourier transform method within the OFT. 61 4.2.1 Frequency aliasing and windowing. 61 4.2.2 Errors due to time aliasing. 62 4.3 Limitations of using the ‘Fourier transform method. resulting from errors in experimental data. 65 4.3.1 Consequences of linear damping model. 65 4.3.2 Accuracy of experimental data. 66 4.3.3 Effect of the out-of-range modes. 68 4.4 Case study - Transient response analysis of a beam. 70 4.5 Discussion. 73 Tables for chapter 4. 75 Figures for chapter 4. 78 Page 5 RESPONSE CHARACTERISTICS OF NON-LINEAR ELEMENTS USING MODAL TESTING TECHNIQUES. 5.0 Introduction. 101 5.1 Some examples of non-linear elements found in practice. 103 5.1 .l Stiffness type non-linearities. 103 5.1.2 Damping type non-linearities. 105 5.2 Frequency response measurement of non-linear elements. 107 5.3 Frequency response characteristics from sine tests. 109 5.3.1 Characteristics in the measured Bode plot. 110 5.3.2 Modal parameters obtained from SDOF analysis. 112 5.3.3 Hilbert transform. 115 5.3.4 Characteristics using ‘standard’ sine excitation. 115 5.4 Response characteristics from impulse tests. 116 5.4.1 Characteristics of the time-histories. 116 5.4.2 Data trends in the frequency domain from impulse excitation. 118 5.5 Comparison of response characteristics in the time domain. 121 5.6 Discussion. 123 Tables for chapter 5. 125 Figures for chapter 5. 136 5 Page 6 TRANSIENT RESPONSE PREDICTION OF NON-LINEAR ELEMENTS USING DATA FROM MODAL TESTS. 6.0 Introduction. 181 6.1 Summary of routes for transient response prediction. 182 6.2 Transient response prediction for a cubic stiffness element. 184 6.3 Transient response prediction for a system with backlash. 187 6.4 Transient response prediction for a system with bi-linear stiffness. 190 6.5 Transient response prediction for a system with friction. 192 6.6 Transient response prediction for an element with quadratic viscous damping. 194 6.7 Discussion. 196 Tables for chapter 6. 197 Figures for chapter 6. 198 7 RESPONSE ANALYSIS OF MDOF SYSTEMS WITH A NON-LINEAR ELEMENT. 7.0 Introduction. 211 7.1 System definition. 212 7.2 Application of prediction techniques for transient response of MDOF non-linear systems. 213 7.3 Modal analysis of non-linear systems. 215 7.4 Transient response of non-linear systems via the frequency domain. 218 7.4 Discussion. 220 Tables for chapter 7. 222 Figures for chapter 7. 232 t Page 8 CONCLUDING DISCUSSION. 8.0 Introduction. 252 8.1 Discussion. 252 8.2 Recommendations for transient response predictions. 256 8.3 Suggestions for further research. 260 9 REFERENCES. 261 10 APPENDICES. Appendix 1 Summary of essential modal theory. 279 Appendix 2 Summary of SDOF modal analysis methods. 284 Appendix 3 MDOF curve fitting for lightly damped structures. 289 Appendix 4 Basic impedance coupling theory. 291 Appendix 5 Free decay for systems with viscous or hysteretic damping. 292 Appendix 6 Determination of friction damping from reciprocal-of-receptance analysis. 294 Appendix 7 Development of a non-linear model for the transient response prediction of a friction element. 296 7 List of tables Page 4.1 Modal parameters for theoretical 12 mode structure. 75 4.2 Modal paramers from FRF data obtained using stepped-sine excitation. 76 4.3 Modal paramers from FRF data obtained using random and impulse excitations. 77 5.1 Trends in frequency domain displays from non-linear systems subjected to sine testing. 125 5.2 Various parameters evaluated from a single constant-force stepped-sine test of a system with cubic stiffness. 126 5.3 Various parameters evaluated from a single constant-force stepped-sine test of a system with backlash. 127 5.4 Various parameters evaluated from a single constant-force stepped-sine test of a system with friction. 128 5.5 Various parameters evaluated from a single constant-force stepped-sine test of a system with quadratic viscous damping. 129 5.6 Trends in frequency domain displays from non-linear systems subjected to impulse excitation. 130 5.7 Various parameters evaluated from a single impulse test of a system with cubic stiffness. 131 5.8 Various parameters evaluated from a system with backlash subjected to an impulse. 132 5.9 Parameters from the ‘modes’ of a bi-linear system subjected to , a single impulse. 133 5.10 Various parameters evaluated from a system with friction subjected to an impulse. 134 5.11 Various parameters evaluated from a system with quadratic viscous damping subjected to an impulse. 135 a Page 6.1 Data from analysis of systems with backlash type non-linearity subjected to constant-force stepped-sine tests and reciprocal- of-receptance analysis using data either above or below resonance and averaging the two results. 197 7.1 Physical description of each 2 degree-of-freedom system. 222 7.2 Parameters from mode 1 point 1 ,l. 223 7.3 Parameters from mode 2 point 1,l. 224 7.4 Parameters from mode 1 point 1,2. 225 7.5 Parameters from mode 2 point 1,2. 226 7.6 Parameters from mode 1 point 2,l. 227 7.7 Parameters from mode 2 point 2,i. 228 7.8 Parameters from mode 1 point 2,2. 229 7.9 Parameters from mode 2 point 2,2. 230 7.10 Results from using ‘Ident ’type analysis of point (2,2) of the 2 degree-of-freedom system with bi-linear stiffness. 231 9 >,I . . . . _j.,‘,,,,.. / . .Iw .: .- List of figures Page 2.1 Shock response spectra for a half-sine pulse. 28 3.1 Bode plot using linear frequency axis and log response. 50 3.2 Nyquist display with frequency information included. 50 3.3 Data from sine test - Coarse log frequency sweep followed by fine linear frequency sweeps around resonance. 51 3.4 Measured FRF from random excitation on a structure, linear frequency spacing over the full frequency range. 51 3.5 Nyquist analysis. 52 3.6 reciprocal-of-receptance analysis. 53 3.7 Effect of MDOF extension to SDOF analysis. 54 3.8 Effect of residuals on regenerated FRF data. 55 4.1 Common windows and their frequency components. 78 4.2 Comparison of time-histories transformed from SDOF modal models with equivalent linear damping. 79 4.3 Comparison of time-histories transformed from SDOF modal models with equivalent linear damping. 80 4.4 Effect of errors in natural frequency on the predicted time-history of a theoretical 12 mode system. 81 4.5 Effect of errors in the magnitude of the modal constant on the predicted time-history of a theoretical 12 mode system. a2 4.6 Effect of errors in the phase of the modal constant on the predicted time-history of a theoretical 12 mode system. 83 4.7 Effect of errors in the damping estimate on the predicted time-history of a theoretical 12 mode system. 84 4.8 Displacement time-histories from a theoretical 12 mode system. 85 4.9 Velocity time-histories from a theoretical 12 mode system. 86 4.10 Acceleration time-histories from a theoretical 12 mode system. 87 4.11 Displacement time-histories from a theoretical 12 mode system: effect of high frequency modes. 88 10 L ,

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convolution and is' primarily applicable to linear models whose impulse The convolution integral as applied to transient vibration analysis is an
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