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Experiment #4 Dynamic Response of a Vibrating Structure to Sinusoidal Excitation
Objectives Perform a standard vibration test to measure the frequency  response of a structural system      1. Solve a differential equation describing the motion of a structure with one degree of freedom under sinusoidal excitation 2. Calculate the equivalent viscous damping coefficient (ฮถ) of a single degree of freedom structure     3.
Test Specimen and Test Setup Exciter Load Cell Accelerometer Specimen
Part I โ€“ Frequency Response Forced Response Free Response Manual Excitation Mechanical Excitation
Forced Response Node First Mode โ€“ 10.1 Hz First Resonance โ€“ displays one node
Forced Response Second Mode โ€“ 68.8 Hz Nodes Second Resonance โ€“ displays two nodes
Forced Response Third Mode โ€“ 115 Hz Nodes Third Resonance โ€“ displays three nodes
Forced Response Before 68.6 Hz Resonance  ๐‘‹๐น0ย is small ย  Force Acceleration In phase
Forced Response Before 68.6 Hz Resonance  ๐‘‹๐น0ย is small ย  Force Acceleration In phase
Forced Response At 68.6 Hz Resonance  ๐‘‹๐น0ย is large ย  Force Acceleration 90ยฐ phase shift
Forced Response After 68.6 Hz Resonance  ๐‘‹๐น0ย is small ย  Force Acceleration Back in phase
Magnitude Ratio vs. Frequency Experimental data indicates that there is a resonance ~ 68 Hz
Phase Angle vs. Frequency Experimental data indicates that there is a phase shift of 90ยฐ at ~68 Hz
Free Response Acceleration Decreasing acceleration and decreasing displacement
Part II โ€“ Lumped Parameter Model   The diagram below describes the motion of our beam:  x F = applied force by the exciter X = beam displacement
Single DOF Spring-Mass-Damper System The mathematical model we used to describe the motion of the beam was a Single DOF Spring-Mass-Damper System.   X(t) = displacement F(t) = applied load  m = mass k = spring constant c = damping coefficient
Single DOF Spring-Mass-Damper System The lumped parameter model can be modeled by a non-homogeneous differential equation: ๐‘š๐‘ฅ+๐‘๐‘ฅ+๐‘˜๐‘ฅ=๐น(๐‘ก) ย  We developed two particular solutions to this DE: ๐œ™=tanโˆ’1โˆ’2๐œ๐œ”๐œ”๐‘›1โˆ’๐œ”๐œ”๐‘›2 ย  - Phase angle between forcing function and the displacement of the beam ๐‘‹๐น0=1๐‘˜1โˆ’๐œ”๐œ”๐‘›22+2๐œ๐œ”๐œ”๐‘›2 ย  - Magnitude ratio of displacement and applied force
Part III โ€“ Equivalent Viscous Damping Coefficient (ฮถ) Three Methods for Finding ฮถ Half-Power Method Log Decrement Method Best Guess Method
Half-Power Method ๐œ๐ป๐‘ƒ=๐‘“2โˆ’๐‘“12๐‘“๐‘› ย  The half-power method utilizes frequencies on either side of the natural frequency along with the natural frequency to approximate the viscous damping coefficient (ฮถ).  ๐œ๐ป๐‘ƒ=69.1142โˆ’68.52952โˆ—68.9 ย  ๐œป๐‘ฏ๐‘ท=๐ŸŽ.๐ŸŽ๐ŸŽ๐Ÿ’๐Ÿ๐Ÿ’๐Ÿ— ย 
Half-Power Method ๐‘‹๐น0 ย 
Log Decrement Method The log decrement method utilizes frequencies at different points along the Free Response result in Part I. ๐›ฟ=1๐‘›ln๐‘ฅ0๐‘ฅ๐‘› ย  -  This is the log decrement The log decrement is then used to find the viscous damping coefficient (ฮถ):  ๐œ๐ฟ๐ท=11+2๐œ‹๐›ฟ2 ย  ๐œ๐ฟ๐ท=11+2๐œ‹0.075972 ย  ๐œป๐‘ณ๐‘ซ=๐ŸŽ.๐ŸŽ๐Ÿ๐Ÿ๐ŸŽ๐Ÿ— ย 
Best Guess Method The Best Guess Method involved simply picking a value for ฮถ and then plotting the theoretical curves alongside the experimental data.  The correct value of ฮถ is found when the theoretical curves match the experimental data. ๐œป๐‘ฉ๐‘ฎ=๐ŸŽ.๐ŸŽ๐Ÿ ย 
Comparison of HP and LD ฮถ Values Differential error analysis shows that: ๐œŽ๐œป๐‘ฏ๐‘ทย =7โˆ—๐œŽ๐œป๐‘ณ๐‘ซย  Therefore, we conclude that the Log Decrement Method is a much more accurate method of calculating the viscous damping coefficient (ฮถ). ย 
Frequency Response Function Curves - Magnitude Magnitude Ratio vs. Frequency, ฯ‰ All curves agree as to the location of the resonant frequency The value of ฮถ affects both the height of the curve and the slope leading up to the resonance 68.6
Frequency Response Function Curves โ€“ Phase Angle (ฯ†) Phase Shift, ฯ† vs. Frequency, ฯ‰ All curves indicate that there is a phase shift of ~90ยฐ at 68.6 Hz FRF curves donโ€™t correlate well with the experimental phase shift in this region 68.6
Conclusions ,[object Object]
 The magnitude ratio curves produced by our model correlate very well with our experimental data.

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Dynamic Response Of A Vibrating Structure To Sinusoidal Excitation

  • 1. Experiment #4 Dynamic Response of a Vibrating Structure to Sinusoidal Excitation
  • 2. Objectives Perform a standard vibration test to measure the frequency response of a structural system 1. Solve a differential equation describing the motion of a structure with one degree of freedom under sinusoidal excitation 2. Calculate the equivalent viscous damping coefficient (ฮถ) of a single degree of freedom structure 3.
  • 3. Test Specimen and Test Setup Exciter Load Cell Accelerometer Specimen
  • 4. Part I โ€“ Frequency Response Forced Response Free Response Manual Excitation Mechanical Excitation
  • 5. Forced Response Node First Mode โ€“ 10.1 Hz First Resonance โ€“ displays one node
  • 6. Forced Response Second Mode โ€“ 68.8 Hz Nodes Second Resonance โ€“ displays two nodes
  • 7. Forced Response Third Mode โ€“ 115 Hz Nodes Third Resonance โ€“ displays three nodes
  • 8. Forced Response Before 68.6 Hz Resonance ๐‘‹๐น0ย is small ย  Force Acceleration In phase
  • 9. Forced Response Before 68.6 Hz Resonance ๐‘‹๐น0ย is small ย  Force Acceleration In phase
  • 10. Forced Response At 68.6 Hz Resonance ๐‘‹๐น0ย is large ย  Force Acceleration 90ยฐ phase shift
  • 11. Forced Response After 68.6 Hz Resonance ๐‘‹๐น0ย is small ย  Force Acceleration Back in phase
  • 12. Magnitude Ratio vs. Frequency Experimental data indicates that there is a resonance ~ 68 Hz
  • 13. Phase Angle vs. Frequency Experimental data indicates that there is a phase shift of 90ยฐ at ~68 Hz
  • 14. Free Response Acceleration Decreasing acceleration and decreasing displacement
  • 15. Part II โ€“ Lumped Parameter Model The diagram below describes the motion of our beam: x F = applied force by the exciter X = beam displacement
  • 16. Single DOF Spring-Mass-Damper System The mathematical model we used to describe the motion of the beam was a Single DOF Spring-Mass-Damper System. X(t) = displacement F(t) = applied load m = mass k = spring constant c = damping coefficient
  • 17. Single DOF Spring-Mass-Damper System The lumped parameter model can be modeled by a non-homogeneous differential equation: ๐‘š๐‘ฅ+๐‘๐‘ฅ+๐‘˜๐‘ฅ=๐น(๐‘ก) ย  We developed two particular solutions to this DE: ๐œ™=tanโˆ’1โˆ’2๐œ๐œ”๐œ”๐‘›1โˆ’๐œ”๐œ”๐‘›2 ย  - Phase angle between forcing function and the displacement of the beam ๐‘‹๐น0=1๐‘˜1โˆ’๐œ”๐œ”๐‘›22+2๐œ๐œ”๐œ”๐‘›2 ย  - Magnitude ratio of displacement and applied force
  • 18. Part III โ€“ Equivalent Viscous Damping Coefficient (ฮถ) Three Methods for Finding ฮถ Half-Power Method Log Decrement Method Best Guess Method
  • 19. Half-Power Method ๐œ๐ป๐‘ƒ=๐‘“2โˆ’๐‘“12๐‘“๐‘› ย  The half-power method utilizes frequencies on either side of the natural frequency along with the natural frequency to approximate the viscous damping coefficient (ฮถ). ๐œ๐ป๐‘ƒ=69.1142โˆ’68.52952โˆ—68.9 ย  ๐œป๐‘ฏ๐‘ท=๐ŸŽ.๐ŸŽ๐ŸŽ๐Ÿ’๐Ÿ๐Ÿ’๐Ÿ— ย 
  • 21. Log Decrement Method The log decrement method utilizes frequencies at different points along the Free Response result in Part I. ๐›ฟ=1๐‘›ln๐‘ฅ0๐‘ฅ๐‘› ย  - This is the log decrement The log decrement is then used to find the viscous damping coefficient (ฮถ): ๐œ๐ฟ๐ท=11+2๐œ‹๐›ฟ2 ย  ๐œ๐ฟ๐ท=11+2๐œ‹0.075972 ย  ๐œป๐‘ณ๐‘ซ=๐ŸŽ.๐ŸŽ๐Ÿ๐Ÿ๐ŸŽ๐Ÿ— ย 
  • 22. Best Guess Method The Best Guess Method involved simply picking a value for ฮถ and then plotting the theoretical curves alongside the experimental data. The correct value of ฮถ is found when the theoretical curves match the experimental data. ๐œป๐‘ฉ๐‘ฎ=๐ŸŽ.๐ŸŽ๐Ÿ ย 
  • 23. Comparison of HP and LD ฮถ Values Differential error analysis shows that: ๐œŽ๐œป๐‘ฏ๐‘ทย =7โˆ—๐œŽ๐œป๐‘ณ๐‘ซย  Therefore, we conclude that the Log Decrement Method is a much more accurate method of calculating the viscous damping coefficient (ฮถ). ย 
  • 24. Frequency Response Function Curves - Magnitude Magnitude Ratio vs. Frequency, ฯ‰ All curves agree as to the location of the resonant frequency The value of ฮถ affects both the height of the curve and the slope leading up to the resonance 68.6
  • 25. Frequency Response Function Curves โ€“ Phase Angle (ฯ†) Phase Shift, ฯ† vs. Frequency, ฯ‰ All curves indicate that there is a phase shift of ~90ยฐ at 68.6 Hz FRF curves donโ€™t correlate well with the experimental phase shift in this region 68.6
  • 26.
  • 27. The magnitude ratio curves produced by our model correlate very well with our experimental data.
  • 28.

Editor's Notes

  1. Second derivative of sin is โ€“sin