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Publication Number:  FHWA-HRT-14-049    Date:  August 2014
Publication Number: FHWA-HRT-14-049
Date: August 2014

 

Mitigation of Wind-Induced Vibration of Stay Cables: Numerical Simulations and Evaluations

CHAPTER 3: PRELIMINARY ANALYSIS OF STAY CABLE VIBRATIONS

INTRODUCTION

This chapter illustrates some common issues on finite element analysis of stay cables using examples. First, single cables with varying degrees of complexity were treated. Then, systems with two stay cables interconnected with a transverse crosstie were analyzed. Finally, a stay cable system in an actual cable-stayed bridge that was previously analyzed by other investigators using a non-FEM was analyzed using FEM, and the results were compared.

For analysis, finite element analysis software SAP2000® was used.(8) Beam elements with appropriate properties were used to model the stay cables and crossties, and the P-delta analysis technique was used to account for the effects of pre-tensioned forces in the stay cables and crossties.

NUMERICAL MODELING AND ANALYSIS OF STAY CABLES

Taut String Model

In the first example, the transverse vibration of a stay cable, modeled as a taut string with fixed ends, was analyzed using FEM and compared with the theoretical solution. The cable had the following fictitious properties:

A beam element with zero flexural stiffness and subjected to axial tension was used to model a taut string. (In practice, a negligibly small number is used for flexural stiffness to avoid numerical instability.)

An illustration of the cable along with the input data and sample results is presented in figure 23. The results from finite element analysis are shown to match theoretical solutions. T1 and T2 denote the period of the first and second mode, respectively. The first 4 vibration mode shapes calculated are shown in figure 24, and the natural vibration frequencies for the first 10 modes are shown in figure 25. The natural frequency is a linear function of the mode number.

This illustration shows a schematic representation of a simple taut string. The values of parameters including the length, pre-tension, and density per unit length of the string are indicated. Also included in the figure are selected analysis results from the theory and finite element analysis. Natural periods for the first two vibration modes of the string computed from these two approaches are presented and compared.
Figure 23 . Illustration. Analysis of a simple taut string.

This image shows the first four vibration mode shapes of a taut string determined from a finite element analysis. Each mode shape exhibits harmonic sinusoidal motions about the axis of the string with a lobe, two lobes, three lobes, and four lobes.
Figure 24 . Image. The first four mode shapes for the vibration of a taut string.

The graph shows the variation of natural vibration frequencies of a taut string as a function of mode number. The x-axis shows mode number ranging from 0 to 10, and the y-axis shows frequency ranging from 0 to 25 Hz. The relationship between the frequency and mode number is linear, and the maximum value of frequency corresponding to a mode number of 10 is approximately 21 Hz.
Figure 25 . Graph. Natural vibration frequencies of a taut string.

Classical Beam

The vibration of an Euler-Bernoulli (or classical) beam with hinge-hinge end conditions was analyzed using FEM and compared with theoretical solutions. The beam has the same length and density as the string model discussed previously. The beam is assumed to have a circular cross section with a diameter of 1 inch (25.4 mm) and is made of steel with a Young's modulus of 2.9E+7 psi (200 GPa).

An illustrative problem with sample input and output data is presented in figure 26. The results from the numerical analysis match the theory. The first 10 natural frequencies are presented in figure 27. The natural frequency of a classical beam is a quadratic function of the mode number, as predicted by the equation in figure 10.

This illustration shows a schematic representation of a classical beam. The values of parameters including the length, pre-tension, density per unit length, Young's modulus, and diameter of the beam are indicated. Also included are selected analysis results from the theory and finite element analysis. Natural periods for the first two vibration modes of the beam computed from the two approaches are compared.
Figure 26 . Illustration. Analysis of a classical beam.

This graph plots the evolution of natural vibration frequencies of a classical beam as a function of mode number. The x-axis shows the mode number ranging from 0 to 10, and the y-axis shows frequency ranging from 0 to 9 Hz. The relationship between the frequency and mode number is nonlinear, and the maximum value of frequency corresponding to a mode number of 10 is approximately 8 Hz.
Figure 27 . Graph. Natural vibration frequencies of a classical beam.

Taut String with Flexural Stiffness

The vibration of a taut string with finite flexural stiffness (or a beam-column) was analyzed. A flexural stiffness parameter (ξ) of 82.4 was computed according to the equation in figure 14, and hinge-hinge end conditions were used. The problem is described schematically in figure 28. Results from numerical analysis match the analytical solutions discussed in the section, "Vibration of Taut Strings with Flexural Stiffness" in chapter 2.

This illustration shows a schematic representation of a taut string with finite flexural stiffness. The values of parameters including the length, pre-tension, density per unit length, Young's modulus, diameter, and flexural stiffness parameter of the cable are indicated. Also included are selected analysis results from the theory and finite element method. Natural periods for the first two vibration modes of the taut string computed from the two approaches are presented and compared.
Figure 28 . Illustration. Analysis of a taut string with finite flexural stiffness and pinned-pinned ends.

The natural frequencies of the taut string with flexural stiffness and those of the taut string without flexural stiffness are shown in figure 29. It can be seen that taking into account the flexural stiffness generally increases the natural frequencies of its transverse vibration. The significance of flexural stiffness, however, is very limited for lower-order vibration modes but picks up noticeably with increasing mode number.

This graph plots the variation of natural vibration frequencies of a taut string with finite flexural stiffness and hinge-hinge supports as a function of mode number. The x-axis shows mode number ranging from 0 to 10, and the y-axis shows frequency ranging from 0 to 25 Hz. The relationship between the frequency and mode number is nonlinear, and the maximum value of frequency corresponding to a mode number of 10 is approximately 22.5 Hz. The result is compared with that of a taut string that produces a linear relationship between the frequency and mode number.
Figure 29 . Graph. Natural vibration frequencies of a taut string with finite flexural stiffness and hinge-hinge supports.

A similar problem with fixed-end conditions was also analyzed. The finite element solutions match those predicted by an approximate formula by Mehrabi and Tabatabai, as seen in figure 30.(6) No closed form solution is known to exist for this problem.

This illustration shows a schematic representation of a taut string with finite flexural stiffness and fixed-fixed end conditions. The values of parameters including the length, pre-tension, density per unit length, Young's modulus, diameter, and flexural stiffness parameter of the cable are indicated. Also included are selected analysis results from a method developed by a contractor and finite element method. Natural periods for the first two vibration modes of the taut string computed from the two approaches are compared.
Figure 30 . Illustration. Analysis of a taut string with finite flexural stiffness and fixed-fixed ends.

In figure 31, the influence of cable end conditions, whether fixed or hinged, on natural frequencies is compared. Relatively small differences are observed between the two cases. However, the differences increase with increasing mode number.

This graph plots the variation of natural vibration frequencies of a taut string with finite flexural stiffness and two different support conditions, hinged-hinged and fixed-fixed, as a function of mode number. The x-axis shows mode number ranging from 0 to 10, and the y-axis shows frequency ranging from 0 to 25 Hz. The relationship between the frequency and mode number is nonlinear in both cases, and a taut string with fixed-fixed end conditions produced slightly greater natural frequencies than that with hinged-hinged end conditions. The maximum values of frequency corresponding to a mode number of 10 are approximately 23 and 22.5 Hz for the fixed-fixed and hinged-hinged end conditions, respectively.
Figure 31 . Graph. Natural vibration frequencies of a taut string with finite flexural stiffness and two different support conditions.

TWO-CABLE SYSTEM WITH CROSSTIE

A simple system of two twin cables interconnected by a cross tie was analyzed (see figure 32). An optional tie to the ground was also considered. Each cable has the same dimensions and properties as the single cable introduced in the previous example (L = 1,000 inches (25.4 m), H = 10 kip (44.5 kN), ρL = 0.222 lbm/inch (3.96 kg/m), D = 1 inch (25.4 mm), fixed-fixed ends). The ties are modeled as an elastic spring, and a number of combinations of stiffness values (K and KG) are considered, where K is the stiffness between two cables, and KG is the stiffness between the cable and the ground or bridge deck.

This illustration shows two stay cables connected with a crosstie and anchored to the ground. The crosstie, with a spring constant of K, connects the two cables at their midpoints, and the system is grounded through a spring with a spring constant of K subscript G. Both cables are of the same length, L, and are under the same tension, H.
Figure 32 . Illustration. Two-cable system with crossties.

First, the in-plane free vibration of this system was analyzed. Figure 33 shows the evolution of the natural frequency of a system when K = 0 and KG = 0 (i.e., when there are no crosstie or anchorage connecting the two cables). Figure 34 shows results when K is finite (K = 0.1 kip/inch (7.5 kN/m)) and KG = 0. It can be seen from figure 34 that the frequencies for n = 2, 6, 10, ... are increased by the presence of a crosstie (spring) between the cables. Figure 35 shows the evolution of mode-frequencies when both K and KG have finite spring constants.

This graph plots the variation of natural vibration frequencies of a two-cable system where stiffness of crosstie between two cables (K) equals 0 and stiffness of crosstie between the cable and ground (K subscript G) equals 0 as a function of mode number. The x-axis shows mode number ranging from 0 to 10, and the y-axis shows frequency ranging from 0 to 14 Hz. The relationship between the frequency and mode number is characterized by a staircase-shaped variation, with a maximum frequency of 10.4 Hz at mode numbers 9 and 10.
Figure 33 . Graph. Mode-frequency evolution for a two-cable system with K = 0 and KG = 0.

This graph plots the variation of natural vibration frequencies of a two-cable system where stiffness of crosstie between two cables (K) equals finite and stiffness of crosstie between the cable and ground (K subscript G) equals 0 as a function of mode number. The x-axis shows mode number ranging from 0 to 10, and the y-axis shows frequency ranging from 0 to 14 Hz. The relationship between the frequency and mode number is characterized by a modified staircase-shaped curve, with the 1st mode frequency being at about 2 Hz and the 10th mode frequency being at 11.1 Hz.
Figure 34 . Graph. Mode-frequency evolution for a two-cable system with K = finite and KG = 0.

This graph plots the variation of natural vibration frequencies of a two-cable system where stiffness of crosstie between two cables (K) equals finite and stiffness of crosstie between the cable and ground (K subscript G) equals finite as a function of mode number. The x-axis shows mode number ranging from 0 to 10, and the y-axis shows frequency ranging from 0 to 14 Hz. The relationship between the frequency and mode number is characterized by a modified staircase-shaped curve, with the 1st mode frequency of 2.5 Hz and the 10th mode frequency of approximately 11.3 Hz.
Figure 35 . Graph. Mode-frequency evolution for a two-cable system with K = finite and KG = finite.

From figure 35, it is apparent that anchoring the crosstie to the ground increases the frequencies (for n = 1, 2, 5, 6, ...) of the two-cable system. Figure 36 shows the evolution of natural frequency of a system when both springs are rigid (K → infinite, KG → infinite). Due to the rigid support of the cables at their midpoints, the first two vibration modes of the unrestrained free cables were suppressed, and thus the first four consecutive modes have the same frequencies, etc.

This graph plots the variation of natural vibration frequencies of a two-cable system where stiffness of crosstie between two cables (K) is approaching infinity and stiffness of crosstie between the cable and ground (K subscript G) is approaching infinity as a function of mode number. The x-axis shows mode number ranging from 0 to 10, and the y-axis shows frequency ranging from 0 to 14 Hz. The relationship between the frequency and mode number is characterized by a wide staircase-shaped curve, with mode frequencies 1-4 coinciding at about 4.2 Hz, mode frequencies 5-8 at about 8.4 Hz, and mode frequencies 9 and 10 at approximately 12.6 Hz.
Figure 36 . Graph. Mode-frequency evolution for a two-cable system with K → infinite and KG → infinite.

Two selected mode shapes from the finite element analysis in comparison with those presented by Caracoglia and Jones are shown in figure 37.(9) The crosstie deforms only for modes n = 2, 6, 10, etc. For all other modes, the crosstie moves as a rigid body. The same parameters (K = 0.1 kip/inch (7.5 kN/m) and KG = 0) as in the case of figure 34 were used. An analytically based and numerically implemented method, which does not involve any finite element procedure, was developed by Caracoglia and Jones and used for the analysis of the in-plane free-vibration of a set of interconnected taut cable elements.(9) The results from the two different approaches are the same.

This image compares the second and sixth mode shapes of a two-cable system determined from the finite element analysis (top) and from Caracoglia and Jones (bottom). The x-axis shows normalized abscissa ranging from 0 to 1, and the y-axis provides an arbitrary scale for amplitudes of a mode shape. The mode shapes from both the finite element analysis and Caracoglia and Jones are noted for their two-way symmetry.
Reprinted with permission from Elsevier
Figure 37 . Image. Comparison of mode shapes from finite element analysis (top) and from Caracoglia and Jones (bottom).(9)

The mode-frequency evolution of a two-cable system with various combinations of crosstie stiffnesses was analyzed and is presented in figure 38. The top enveloping curve corresponds to the case with a rigid crosstie and a rigid ground tie. The bottom enveloping curve corresponds to the case with no crosstie and no ground tie. The two other cases fall in between these two extreme cases, and the corresponding mode-frequency evolution curves stay within the top and bottom enveloping curves of these two extreme cases. The curves clearly show the stiffening effect of the crosstie and anchorage, resulting in increased natural frequencies of the system.

This graph plots the variation of natural vibration frequencies of a two-cable system with various combinations of crosstie and anchorage stiffnesses as a function of mode number. Four different combinations are considered: zero crosstie stiffness and zero anchorage stiffness, a finite crosstie stiffness and zero anchorage stiffness, a finite crosstie stiffness and infinite anchorage stiffness, and an infinite crosstie stiffness and infinite anchorage stiffness. The x-axis shows mode number ranging from 0 to 10, and the y-axis shows frequency ranging from 0 to 14 Hz. The four curves generally trend from the lower left to the upper right.
Figure 38 . Graph. Mode-frequency evolution for a two-cable system with various combinations of crosstie stiffnesses.

FULL-SCALE STAY CABLE NETWORK

Vibration Mode Shapes

Analysis was extended to a real full-scale cable network. The Fred Hartman Bridge in Houston, TX, was selected for illustration and comparison purposes. Photos of the bridge and cable network are presented in figure 39 and figure 40, respectively. The results from finite element analysis are compared with those from the analytical method by Caracoglia and Jones wherever possible.(10)

This photo shows the Fred Hartman Bridge in Houston, TX. Taken from land, it shows the diamond-shaped towers that support the stay cable system and the main and side spans of the bridge.
Figure 39 . Photo. Fred Hartman Bridge in Houston, TX.

This photo shows the stay cable network that supports the Fred Hartman Bridge in Houston, TX. Taken from the bridge deck, it shows a series of cables rising up from the deck to towers in the distance.
Figure 40 . Photo. The cable network of the Fred Hartman Bridge in Houston, TX.

Finite element discretization of a network of main-span stay cables (A-line) of the Fred Hartman Bridge is shown in figure 41. The stay cables are interconnected with three lines of crossties. The configuration shown represents an equivalent two-dimensional (2D) network reduced by Caracoglia and Jones from the original three-dimensional (3D) network.(10) The analytical method developed by Caracoglia and Jones is designed for 2D networks, whereas finite element analysis simulates up to 3D configurations. For comparison purposes, however, the 2D equivalent network generated by Caracoglia and Jones is used here. Analysis is confined to the in-plane free vibration of the network.

This image shows a two-dimensional finite element model of the Fred Hartman Bridge stay cable system. The stay cables broken into segments by crossties are modeled using beam elements, and the crossties are modeled using spring elements. The beam elements are indicated by discrete symbols along the cables. The ends of the cables are supported either on a hinge or roller, and the ends of crossties are fixed to a cable. The crossties divide the longest cable into four equal segments.
Figure 41 . Image. Finite element model for the stay cable system of the Fred Hartman Bridge in Houston, TX.

The first four in-plane vibration mode shapes of the cable network from the finite element analysis and from Caracoglia and Jones are shown in figure 42. The mode shapes from these two different calculations are the same. Some minute discrepancies are attributed to intrinsic differences in the analysis procedure of the two approaches. The modes shown in figure 42 are global in nature in that the majority of the cable segments participate in the oscillation. For n = 1 and 2, modes are clearly global. However, for n = 3 and 4, some local behaviors are superimposed on global behaviors.

This image compares the vibration mode shapes of the Fred Hartman Bridge stay cable system in the first four modes from the finite element analysis to the method from Caracoglia and Jones. In both finite element analysis and the method from Caracoglia and Jones, the first three modes are characterized by global motion in which most of the cable segments are involved in vibration. A localized vibration mode appears to develop at the fourth mode in which only a few cable segments show a dominant movement, while the rest remain fairly stationary.
Reprinted with permission from Elsevier
Figure 42 . Image. First four vibration mode shapes of the Fred Hartman Bridge stay cable system from finite element analysis (top) and from Caracoglia and Jones (bottom).(10)

As the mode number increases, local modes, in which the response of the network is limited to some intermediate segments of cables, become evident. Figure 43 shows mode shapes for n = 5–8. The wavelengths in these vibration modes are dictated by the distances between two adjacent crossties. Subsequent vibration modes, densely populated in frequency, are seen to be a permutation of a similar pattern dominated by a few cables. Local modes are found to dominate for up to n = 28.

This image compares the vibration mode shapes of the Fred Hartman Bridge stay cable system in the fifth to eighth modes from the finite element analysis to the method from Caracoglia and Jones. For both methods, these mode shapes are all characterized by localized motion in which only a limited number of cable segments are involved in motion, while the rest of the cable system remains quite stationary.
Reprinted with permission from Elsevier
Figure 43 . Image. Vibration mode shapes 5–8 of the Fred Hartman Bridge stay cable system from finite element analysis (top) and from Caracoglia and Jones (bottom).(10)

However, a second set of global network modes occurred at n = 29 and continued for a few modes and then local modes resumed. This global-local pattern repeats thereafter. Figure 44 shows mode shapes for n = 29–32. Global modes of vibration are noticeable for n = 29–31, and thereafter, local modes resumed.

This image compares the vibration mode shapes of the Fred Hartman Bridge stay cable system in the 29th to 32nd modes from the finite element analysis in comparison to the Caracoglia and Jones method. In both methods, modes 29 to 31 are characterized by global modes, and a localized mode resumes at mode 32.
Reprinted with permission from Elsevier
Figure 44 . Image. Vibration mode shapes 29–32 of the Fred Hartman Bridge stay cable system from finite element analysis (top) and from Caracoglia and Jones (bottom).(10)

Mode-Frequency Evolution

The modal characteristics of the network are illustrated in figure 45 in the mode-frequency evolution chart where the natural frequency of the network is plotted as a function of the mode number.


This graph shows the variation of the natural frequencies of a networked cable system as a function of the mode number for the Fred Hartman Bridge as determined from the finite element analysis. The network behavior is also compared with the behavior of two individual cables, the longest and the shortest ones. The x-axis shows the mode number ranging from 0 to 35, and the y-axis shows frequency ranging from 0.5 to 4.5 Hz. The variation is characterized by a rapid increase of frequency with mode numbers 0 to 3, followed by a plateau region in which the frequency is densely populated over a narrow frequency band for mode numbers 3 to 27. The frequency then increases rapidly again with mode numbers 28 to 30. Another region of plateau appears after that. The frequencies of the network vary from about 1.0 to 4.1 Hz over the range of mode numbers covered in the plot.
Figure 45 . Graph. Mode-frequency evolution for the Fred Hartman Bridge stay cable system from finite element analysis.

The figure shows that a sequence of global modes are followed by a plateau of densely populated local modes, which is then followed by a second set of global modes, etc. This pattern of consecutive steps is typical of the modal behavior of a cable network. Figure 45 shows that the fundamental frequency (n = 1) of the network is bracketed between the fundamental frequencies of the longest and shortest cables. The presence of crossties is seen to enhance the overall performance of the network by increasing their natural frequencies, especially those of global modes. However, analysis also suggests that the presence of crossties may not necessarily be beneficial at plateau frequencies due to potentially undesirable effects associated with densely populated local modes.

The mode-frequency evolution chart generated by Caracoglia and Jones is presented in figure 46 for comparison.(10) The finite element results presented in figure 45 correspond to their analysis case, "NET_3C." Overall, the results from both approaches are the same.

This graph shows the natural frequencies plotted as a function of the mode number and compared to individual cable behavior for the Fred Hartman Bridge presented by Caracoglia and Jones. The x-axis shows the mode number from 0 to 35, and the y-axis shows frequency ranging from 0.5 to 4.5 Hz. The lower limit of the plateau frequency interval is 1.9 Hz, while the upper limit is 2.7 Hz. The graph shows a high-density pattern from modes 0 to 5 up to a frequency of 4.5 Hz for the localized modes. The three comparative cases for network vibration are the original configuration, rigid transverse links, and modified non-rigid configuration with ground restrainers that essentially overlap in the graph. The consecutive step pattern changes at the lower and upper frequency interval plateaus (1.9 and 2.7 Hz, respectively).
Reprinted with permission from Elsevier
Figure 46 . Graph. Mode-frequency evolution for the Fred Hartman Bridge stay cable system.(10)

Variations in Crosstie Configuration

As a modification to the original configuration, two shorter crossties were tied to the ground (i.e., the deck), as shown in figure 47. The resulting mode shapes (for n = 1 and 2) are presented in figure 48. The first mode is quite similar to that of the previous (reference) network. However, the second mode is rather different from the case of the reference network due to anchoring of the middle line of crosstie.

This image shows a two-dimensional finite element model of the Fred Hartman Bridge stay cable system with some crossties anchored to the deck. The stay cables broken into segments by the crossties are modeled using beam elements, and the crossties are modeled using the spring elements. The beam elements are indicated by discrete symbols along the cables. The ends of the cables are supported either on a hinge or roller, and the ends of crossties are fixed either to a cable or the deck. The crossties are spaced equally about one-fourth the distance along the longest cable.
Figure 47 . Image. Finite element model for the stay cable system with some crossties anchored to the deck.

This image compares the vibration mode shapes of the Fred Hartman Bridge stay cable system shown in figure 47 in the first two modes from the finite element analysis compared to the Caracoglia and Jones method. In both methods, the modes are characterized by global motion in which most of the cable segments are involved in vibration.
Reprinted with permission from Elsevier
Figure 48 . Image. First two vibration mode shapes for the model shown in figure 47 from finite element analysis (top) and from Caracoglia and Jones (bottom).(10)

The effect of crosstie anchoring was examined in terms of the mode-frequency evolution behavior, which is shown in figure 49. The addition of grounding ties significantly increased the frequencies of global modes but did not increase the frequencies of local modes by a significant amount. Grounding of crossties apparently made the network stiffer with respect to its global behavior, but it practically did not affect the local vibration responses of individual cables.

This graph compares the evolution of natural frequencies of a networked cable system of the Fred Hartman Bridge for two different crosstie designs, the reference crosstie design and a variation of it. The variation version involves two crosstie lines anchored to the bridge deck as discussed in figure 47. The x-axis shows the mode number ranging from 0 to 35, and the y-axis shows frequency ranging from 0.5 to 4.5 Hz. The stay network with anchored crossties behaves quite similarly to that of the reference design except that the anchored system presents higher natural frequencies for global modes of vibration than the reference design. The frequencies of the modified network vary from about 1.15 to 4.2 Hz over the range of mode numbers covered in the plot.
Figure 49 . Graph. Comparison of mode-frequency evolution for models shown in figure 41 (reference) and figure 47.

As another fictitious variation to the original configuration, the geometry of the two shorter restrainers was modified, as shown in figure 50. This modification helps avoid excessive stretch of the segments of some cables due to the grounding of crossties. This modification would avoid undesirable stress concentrations in these cable segments.

This image shows a two-dimensional finite element model of the Fred Hartman Bridge stay cable system with a varied crosstie configuration, referred to as variation 1. The stay cables broken into segments by the crossties are modeled using beam elements, and the crossties are modeled using spring elements. The beam elements are indicated by discrete symbols along the cables. The ends of the cables are supported either on a hinge or roller, and the ends of crossties are fixed to a cable. The crossties are spaced equally about one-fourth the distance along the longest cable and are curvilinear.
Figure 50 . Image. Finite element model for the stay cable system with a varied crosstie configuration (variation 1).

The first four vibration mode shapes for this variation are shown in figure 51, and the mode-frequency evolution is shown in figure 52. This variation renders slightly lower frequencies of global modes and yet somewhat higher frequencies of local modes. The step behavior of the original configuration is slightly rounded. Comparing figure 51 with figure 42 suggests an improvement of this variation over the original configuration by avoiding the presence of very short segments of cables.

This image shows the first four mode shapes of the Fred Hartman Bridge stay cable system with a crosstie design discussed in figure 50 computed from finite element analysis. The first three modes are characterized by global motion in which most of the cable segments are involved in vibration. A localized vibration mode develops at the fourth mode in which only a few cable segments show a dominant movement, while the rest remain quite stationary.
Figure 51 . Image. Vibration mode shapes 1–4 for the model shown in figure 50.

This graph compares the evolution of natural frequencies of a networked cable system of the Fred Hartman Bridge for two different crosstie designs, the reference crosstie design and design variation 1. The variation version involves the crosstie lines curvilinear in contrast to straight lines of the reference design. The x-axis shows the mode number ranging from 0 to 35, and the y-axis shows frequency ranging from 0.5 to 4.5 Hz. The stay network with crosstie variation 1 produced slightly higher natural frequencies than the reference design for most of the vibration modes, except in the first few modes and the last few modes covered in the figure. The frequencies of the network with variation 1 crosstie design vary from about 0.8 to 3.8 Hz over the range of mode numbers covered in the plot.
Figure 52 . Graph. Comparison of mode-frequency evolution for models shown in figure 41 (reference) and figure 50.

The third variation to the original crosstie configuration involves only a single line of crossties as shown in figure 53. Figure 54 shows the first four mode shapes of this variation, and figure 55 shows the corresponding mode-frequency evolution (in solid diamonds) in contrast to that of the reference configuration. Clearly, it can be seen that the single line of crossties provides less reinforcement to the cable system. More frequent global-local steps occur as the quantity of crossties is reduced.

This image shows a two-dimensional finite element model of the Fred Hartman Bridge stay cable system with a varied crosstie configuration, referred to as variation 2. The stay cables broken into segments by the crossties are modeled using beam elements, and the crossties are modeled using the spring elements. The beam elements are indicated by discrete symbols along the cables. The ends of the cables are supported either on a hinge or roller, and the ends of crossties are fixed to a cable. The single crosstie line bisects the longest cable.
Figure 53 . Image. Finite element model for the stay cable system with a single crosstie line (variation 2).

This image shows the first four mode shapes of the Fred Hartman Bridge stay cable system with a crosstie design discussed in figure 53 computed from finite element analysis. The first mode is characterized by global motion in which most of the cable segments are involved in vibration. In vibration mode shapes 2 through 4, a localized vibration mode is present.
Figure 54 . Image. Vibration mode shapes 1–4 for the model shown in figure 53.

This graph compares the evolution of natural frequencies of a networked cable system of the Fred Hartman Bridge for two different crosstie designs, the reference crosstie design and design variation 2. The variation version involves a single crosstie line in contrast to three lines of the reference design. The x-axis shows the mode number ranging from 0 to 35, and the y-axis shows frequency ranging from 0.5 to 4.5 Hz. The stay network with crosstie variation 2 produces much lower natural frequencies than the reference design for most of the vibration modes. The frequencies of the network with variation 2 crosstie design vary from about 0.9 to 3.4 Hz over the range of mode numbers covered in the plot.
Figure 55 . Graph. Comparison of mode-frequency evolution for models shown in figure 41 (reference) and figure 53.

Finally, the mode-frequency evolution behavior of the original network over extended mode numbers (up to n = 100) is shown in figure 56. Multiple repeated global-local behaviors can be seen.

This graph shows the evolution of natural frequencies of a networked cable system of the Fred Hartman Bridge over an extended range of mode numbers. The x-axis shows the mode number ranging from 0 to 100, and the y-axis shows frequency ranging from 0.0 to 10.0 Hz. The frequencies of the network vary from about 1.0 to 8.8 Hz over the range of mode numbers covered in the plot.
Figure 56 . Graph. Mode-frequency evolution for higher mode numbers.