# Progressive Collapse Analysis of Latticed Telecommunication Towers under Wind Loads

Authors: Shan Gao; Sheliang Wang
Journal: Advances in Civil Engineering
 (2018)

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## Abstract

As the antenna-supporting structures, latticed telecommunication steel towers are considered as critical members of telecommunication infrastructures. It is necessary to perform progressive collapse analysis of lattice telecommunication towers under wind loads. The present study conducts a nonlinear dynamic analysis on 50 m high typical standard latticed telecommunication tripole tower and angle tower by alternative load path method. The finite element models for two towers subjected to design wind loads are developed by ABAQUS. The analysis results show that, for 50 m high standard tripole tower, the member failure in the first three tower sections from tower top would not trigger the collapse of the tower. From the fourth tower section to tower bottom, the member failure at certain wind direction may cause a collapse. For 50 m high standard angle tower, the single member failure in any tower section would not cause the collapse of the tower. A dynamic sensitivity index is proposed to identify the most unfavorable wind direction for tripole tower and angle tower. A progressive collapse fragile curve based on collapse probability of telecommunication tower under wind loads is proposed to assess the anticollapse performance of the towers.


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## Body

## 1. Introduction

Progressive collapse is a chain failure that propagated vertically or horizontally in structures which is caused by a local structural damage under additional loads. Due to the unpredictability of additional loads, the anticollapse design is not quantitatively considered in the structural design until the notorious terrorist attack on the World Trade Center. In order to protect the important buildings from terrorist attacks or other additional loads, a series of standards and codes are issued to assess and diminish the potential of progressive collapse in structures [1–3].The continuing growth of communities requires the expansion of telecommunication networks. Reliable and noninterruptible telecommunication signals are crucial, especially under the natural disaster or terrorist attack. As the antenna-supporting structures, latticed steel towers are considered as a lifeline project in telecommunication engineering. A good assessment for the structural response of latticed telecommunication towers under additional loads is essential for the safety of telecommunication engineering.Due to the numerous amount and construction repeatability of telecommunication towers, the potential danger and flaws in the design tend to be neglected by designers and engineers. Telecommunication towers operate in outdoor natural environment for a long period, in which case the work condition varies greatly and the accidental loads are hard to predict. The safety of the telecommunication towers is threatened by many factors, such as extreme weather or vandalism. Based on the geological and climatic conditions, additional considerations are required in the design of telecommunication towers [4, 5]. The antenna-supporting towers normally involve guyed masts, monopole towers, and latticed towers. The collapse of guyed mast and monopole towers is mostly due to the rupture of guys or overall overturning. The reasons for the collapse of latticed towers are more complicated. It is necessary to perform progressive collapse analysis of lattice telecommunication towers under design loads and accidental loads.Alternative path method (APM) is widely adopted in the anticollapse design and analysis of structures, especially frame structures. This methodology involves the identification of key structural elements and the assessment on remainder of the structure after element removal. According to the importance of the structure, linear static analysis, nonlinear static analysis, linear dynamic analysis, and nonlinear dynamic analysis are adopted to perform the assessment for the potential to progressive collapse. Nonlinear dynamic analysis is the most practical method whilst linear static analysis is the easiest to implement. A dynamic increase factor (DIF) is commonly used in linear static analysis to make the assessment more realistic. The susceptibility and redundancy analysis of progressive collapse in structures are also based on APM. By introducing the susceptibility or redundancy index, the key structural members could be identified by APM.Several studies have been performed on the progressive collapse of structures through APM. Powell compared the results obtained by different analysis procedures and concluded that using dynamic increase factor of 2.0 in linear static analysis may be conservative [6]. In addition, the research conducted by Ruth et al. also showed that the value of 1.5 was suitable for linear static analysis of steel frame structures considering dynamic effect [7]. Kim and Kim performed APM on steel frame structures whose results showed that nonlinear dynamic analysis would result in larger responses in structures than static analysis [8]. Fu developed a 3-D model for steel frame with concrete slab. The results of the research based on this model showed that the removal of the column at a low elevation was more likely to trigger progressive collapse than that of the column at a high elevation [9]. Khandelwal and El-Tawil investigated the robustness of structures by using “pushdown analysis.” The results showed that the dynamic increase factor of 2.0 was significantly higher than the actual value in the study [10]. Song et al. developed both 2-D and 3-D models for steel frame structures. The results of progressive collapse analysis indicated that 3-D finite element model was more accurate than 2-D finite element model in presenting the behavior of the structure in the scenario of column loss [11]. El Kamari et al. simulated the failure of Roissy Charles de Gaulle Airport and pointed out that the defective construction and irrational design in the project resulted in the collapse [12]. Gerasimidis and Sideri proposed a new partial-distributed damage method for steel moment frames. The results showed that local failure in the system can remarkably change the collapse response of the structure [13]. Asgarian et al. conducted a progressive collapse analysis of a lattice transmission tower by using APM. A capacity-to-demand ratio was proposed to identify the key elements. The study also showed that power transmission towers may avoid from progressive collapse under single element damage, due to the adequate alternative load paths [14].The study in this paper aims at assessing the sensitivity of typical latticed telecommunication towers to progressive collapse. ABAQUS [15] is implemented to develop finite element (FE) model for the towers. The latticed towers are subjected to design wind loads. Nonlinear dynamic analysis is conducted on typical standard tripole tower and angle tower by alternative load path method. A dynamic sensitivity index and a collapse probability are both proposed to evaluate the potential to progressive collapse of latticed telecommunication tower.


## 2. Development and Validation of FE Model

### 2.1. Prototype Structures

Unlike the design of building structures, the design of telecommunication towers which is labor-intensive shows the characteristic of repeatability and similarity. In order to improve design efficiency, the Chinese government issues a set of standard design drawings for telecommunication towers, namely, “Drawing Collection of Telecommunication Steel Tower (DCTST)” in the year of 2014 [16]. From then on, all new telecommunication steel towers in China are built referring to DCTST, except in special cases.A standard tripole tower and a standard angle tower from DCTST are chosen as prototype structures. The total height of two towers is 55 m including a 5 m height lightning rod. The general configuration of the towers is shown in Figure1. The right column of numbers in the figures shows the number of each tower section. Tripole tower consists of three pole-legs whilst angle tower consists of four angle-legs. Four platforms are installed on both towers. Each platform carries six sets of antennas. Member sections of the towers are listed in Tables 1 and 2. Chinese grade Q345 structural steel is used for all steel members.Figure 1
Geometry of the prototype towers (mm). (a) Tripole tower; (b) angle tower.
(a)
(b)Table 1
Member sections of tripole tower (mm).
Tower section number
1
2
3
4
5
6
7
8
9
10
Leg member section
Φ89∗5
Φ114∗5
Φ146∗6
Φ159∗8
Φ180∗10
Φ194∗10
Φ219∗10
Φ219∗12
Φ219∗12
Φ219∗12
Cross-brace member section
L50∗5
L63∗5
L70∗5
L70∗5
L70∗5
L70∗5
L80∗6
L80∗6
L80∗6
L80∗6Table 2
Member sections of angle tower (mm).
Tower section number
1
2
3
4
5
6
7
8
9
Leg member section
L80∗6
L100∗8
L125∗10
L140∗12
L160∗14
L180∗16
L180∗16
L200∗16
L200∗18
Cross-brace member section
L63∗5
L63∗5
L63∗5
L70∗5
L75∗6
L80∗6
L90∗7
L90∗7
L100∗7


### 2.2. Development of FE Model

Two 3-D nonlinear FE models of the prototype towers are developed by using ABAQUS as shown in Figure2. Antennas, platforms, and other accessories are all included in the models. ∗Truss elements (T3D2) and ∗Beam elements (B31) from ABAQUS library are adopted to simulate cross-brace members and leg members. Antennas, platforms, and other accessories are modeled by ∗solid elements (C3D8R). Ends of the cross braces with two bolts are assumed to be pin connections. Steel stress-strain relationship is as shown in Figure 2(c). Elastic modulus of 206 GPa, yield stress of 345 MPa, and strain hardening of 1% are assigned for the material properties of steel. Four-leg feet of the model are fixed on the ground.Figure 2
Finite element model. (a) Tripole tower; (b) angle tower; (c) steel stress-strain relationship.


### 2.3. Validation of FE Model

In order to validate the finite element models in Figure2, modal analysis is conducted by ABAQUS and SAP2000 at the same time. The comparison of natural vibration frequencies is shown in Table 3. It can be seen that the difference between the results of the first five modes is within 1% which proves the accuracy of the models.Table 3
Comparison of natural vibration frequencies.
Mode
1
2
3
4
5
Tripole tower
Frequency (Hz)
ABAQUS
1.3010
1.3011
2.6352
2.6354
3.2713
SAP2000
1.3155
1.3165
2.7095
2.7098
3.1850
Angle tower
Frequency (Hz)
ABAQUS
2.2200
2.2226
2.5869
2.5873
5.7509
SAP2000
2.2647
2.2649
2.6095
2.6098
6.8850


## 2.1. Prototype Structures

Unlike the design of building structures, the design of telecommunication towers which is labor-intensive shows the characteristic of repeatability and similarity. In order to improve design efficiency, the Chinese government issues a set of standard design drawings for telecommunication towers, namely, “Drawing Collection of Telecommunication Steel Tower (DCTST)” in the year of 2014 [16]. From then on, all new telecommunication steel towers in China are built referring to DCTST, except in special cases.A standard tripole tower and a standard angle tower from DCTST are chosen as prototype structures. The total height of two towers is 55 m including a 5 m height lightning rod. The general configuration of the towers is shown in Figure1. The right column of numbers in the figures shows the number of each tower section. Tripole tower consists of three pole-legs whilst angle tower consists of four angle-legs. Four platforms are installed on both towers. Each platform carries six sets of antennas. Member sections of the towers are listed in Tables 1 and 2. Chinese grade Q345 structural steel is used for all steel members.Figure 1
Geometry of the prototype towers (mm). (a) Tripole tower; (b) angle tower.
(a)
(b)Table 1
Member sections of tripole tower (mm).
Tower section number
1
2
3
4
5
6
7
8
9
10
Leg member section
Φ89∗5
Φ114∗5
Φ146∗6
Φ159∗8
Φ180∗10
Φ194∗10
Φ219∗10
Φ219∗12
Φ219∗12
Φ219∗12
Cross-brace member section
L50∗5
L63∗5
L70∗5
L70∗5
L70∗5
L70∗5
L80∗6
L80∗6
L80∗6
L80∗6Table 2
Member sections of angle tower (mm).
Tower section number
1
2
3
4
5
6
7
8
9
Leg member section
L80∗6
L100∗8
L125∗10
L140∗12
L160∗14
L180∗16
L180∗16
L200∗16
L200∗18
Cross-brace member section
L63∗5
L63∗5
L63∗5
L70∗5
L75∗6
L80∗6
L90∗7
L90∗7
L100∗7


## 2.2. Development of FE Model

Two 3-D nonlinear FE models of the prototype towers are developed by using ABAQUS as shown in Figure2. Antennas, platforms, and other accessories are all included in the models. ∗Truss elements (T3D2) and ∗Beam elements (B31) from ABAQUS library are adopted to simulate cross-brace members and leg members. Antennas, platforms, and other accessories are modeled by ∗solid elements (C3D8R). Ends of the cross braces with two bolts are assumed to be pin connections. Steel stress-strain relationship is as shown in Figure 2(c). Elastic modulus of 206 GPa, yield stress of 345 MPa, and strain hardening of 1% are assigned for the material properties of steel. Four-leg feet of the model are fixed on the ground.Figure 2
Finite element model. (a) Tripole tower; (b) angle tower; (c) steel stress-strain relationship.


## 2.3. Validation of FE Model

In order to validate the finite element models in Figure2, modal analysis is conducted by ABAQUS and SAP2000 at the same time. The comparison of natural vibration frequencies is shown in Table 3. It can be seen that the difference between the results of the first five modes is within 1% which proves the accuracy of the models.Table 3
Comparison of natural vibration frequencies.
Mode
1
2
3
4
5
Tripole tower
Frequency (Hz)
ABAQUS
1.3010
1.3011
2.6352
2.6354
3.2713
SAP2000
1.3155
1.3165
2.7095
2.7098
3.1850
Angle tower
Frequency (Hz)
ABAQUS
2.2200
2.2226
2.5869
2.5873
5.7509
SAP2000
2.2647
2.2649
2.6095
2.6098
6.8850


## 3. Finite Element Modeling Technique

### 3.1. Loads

Gravity loads at the model are considered by assigning density to structural members, antennas, platforms, and other accessories. Horizontal wind loads are calculated by (1) according to the Chinese Load code for the design of building structures [17]:(1)wk=βzμsμzw0,where w0 stands for the reference wind pressure; βz for the gust effect factor; μs for the topographic factor; and μz for the velocity pressure coefficient.The reference wind pressurew0 for two towers in this study, namely, the design wind pressure in DCTST, is 0.65 kN/m2. The wind loads as shown in Table 4 are applied as concentrated forces at the top of each tower section. The additional values in Table 4 are the wind loads sustained by the platform. There loads are applied to the tower section by which the platform is supported. Based on the appearance of the chosen towers, wind directions are selected for two towers as shown in Figure 3. The applied wind loads in the façade view is shown in Figure 3(c).Table 4
Wind loads (kN).
1
2
3
4
5
6
7
8
9
10
Tripole tower
6.8
9.5 + 12
9.3 + 10.5
8.9 + 9.0
10.9 + 7.7
10.7
10.2
8.0
6.8
6.8
Angle tower
9.4 + 18
11.5 + 15.5
11.3 + 13.5
12.7 + 11.5
18.8
12.8
9.4
9.3
9.1
—Figure 3
Wind directions. (a) Tripole tower; (b) angle tower; (c) façade view (kN).The gravity loads of antennas, platform, and other accessories on each platform are as shown in Table5 according to DCTST. Live loads on platform are adopted as 1.0 kN/m. The vertical load combination on platform is used in the analysis as follows:(2)Load=DL+0.25LL,where DL and LL stand for gravity loads and live loads, respectively.Table 5
Gravity loads on each platform (kN).
From top
1st
2nd
3rd
4th
Tripole tower
32
32
32
40
Angle tower
36
40
50
66


### 3.2. Alternative Path Method

A nonlinear dynamic analysis based on alternative path method is conducted by three steps as follows: (a) Horizontal wind loads are applied at the model in a static analysis step; (b) the structural member is removed over a predefined period in a dynamic analysis step; and (c) the dynamic response of the remaining model is monitored until the model is stabilized in a dynamic analysis step.According to GSA guideline, a failure period which is no more than 1/10 of the period associated with the structural response mode is recommended in the member removal step. According to the natural vibration frequencies in Table3, 0.07 s and 0.05 s of failure period are adopted for tripole tower and angle tower, respectively.In dynamic analysis, Rayleigh damping is employed to create the damping matrix of the model. The typical Rayleigh damping matrix is as follows:(3)C=αM+βK,where M and K stand for mass matrix and stiffness matrix of the structure, respectively, and α and β stand for the mass damping coefficient and the stiffness damping coefficient, respectively.The coefficientα and β which are derived from (4) are introduced into ABAQUS to determine the damping matrix of the model.(4)α=ξ2ω1ω2ω1+ω2β=ξ2ω1+ω2,where ω1 and ω2 stand for the first-order and second-order natural vibration frequency, respectively, and ξ for the damping ratio which is 0.02 for steel structures.


### 3.3. Defined Failure Scenarios

Three pole-legs in tripole tower are numbered as shown in Figure4(a). For wind direction Tri-A and Tri-B, the failure of leg members in pole-leg 1 is most unfavorable. For wind direction Tri-C, the failure of leg members in pole-leg 2 and 3 are both analyzed. From elevation view, the bottom leg member of each tower section is removed notionally as shown in Figure 4(b), namely, ten failure scenarios for each pole-leg.Figure 4
Positions of leg member removal at tripole tower. (a) Plan view; (b) elevation view (take section 9 and 10 for example).
(a)
(b)Figure5(a) shows the number of angle-legs and the corresponding wind direction. For wind direction Ang-A, angle-leg 1 and 2 are chosen to analyze due to the symmetrical arrangement. Angle-leg 1 and 3 would be considered in the analysis for wind direction Ang-B. Nine failure scenarios are defined for each angle-leg as shown in Figure 5(b).Figure 5
Positions of leg member removal at angle tower. (a) Plan view; (b) elevation view (take section 9 and 10 for example).
(a)
(b)


## 3.1. Loads

Gravity loads at the model are considered by assigning density to structural members, antennas, platforms, and other accessories. Horizontal wind loads are calculated by (1) according to the Chinese Load code for the design of building structures [17]:(1)wk=βzμsμzw0,where w0 stands for the reference wind pressure; βz for the gust effect factor; μs for the topographic factor; and μz for the velocity pressure coefficient.The reference wind pressurew0 for two towers in this study, namely, the design wind pressure in DCTST, is 0.65 kN/m2. The wind loads as shown in Table 4 are applied as concentrated forces at the top of each tower section. The additional values in Table 4 are the wind loads sustained by the platform. There loads are applied to the tower section by which the platform is supported. Based on the appearance of the chosen towers, wind directions are selected for two towers as shown in Figure 3. The applied wind loads in the façade view is shown in Figure 3(c).Table 4
Wind loads (kN).
1
2
3
4
5
6
7
8
9
10
Tripole tower
6.8
9.5 + 12
9.3 + 10.5
8.9 + 9.0
10.9 + 7.7
10.7
10.2
8.0
6.8
6.8
Angle tower
9.4 + 18
11.5 + 15.5
11.3 + 13.5
12.7 + 11.5
18.8
12.8
9.4
9.3
9.1
—Figure 3
Wind directions. (a) Tripole tower; (b) angle tower; (c) façade view (kN).The gravity loads of antennas, platform, and other accessories on each platform are as shown in Table5 according to DCTST. Live loads on platform are adopted as 1.0 kN/m. The vertical load combination on platform is used in the analysis as follows:(2)Load=DL+0.25LL,where DL and LL stand for gravity loads and live loads, respectively.Table 5
Gravity loads on each platform (kN).
From top
1st
2nd
3rd
4th
Tripole tower
32
32
32
40
Angle tower
36
40
50
66


## 3.2. Alternative Path Method

A nonlinear dynamic analysis based on alternative path method is conducted by three steps as follows: (a) Horizontal wind loads are applied at the model in a static analysis step; (b) the structural member is removed over a predefined period in a dynamic analysis step; and (c) the dynamic response of the remaining model is monitored until the model is stabilized in a dynamic analysis step.According to GSA guideline, a failure period which is no more than 1/10 of the period associated with the structural response mode is recommended in the member removal step. According to the natural vibration frequencies in Table3, 0.07 s and 0.05 s of failure period are adopted for tripole tower and angle tower, respectively.In dynamic analysis, Rayleigh damping is employed to create the damping matrix of the model. The typical Rayleigh damping matrix is as follows:(3)C=αM+βK,where M and K stand for mass matrix and stiffness matrix of the structure, respectively, and α and β stand for the mass damping coefficient and the stiffness damping coefficient, respectively.The coefficientα and β which are derived from (4) are introduced into ABAQUS to determine the damping matrix of the model.(4)α=ξ2ω1ω2ω1+ω2β=ξ2ω1+ω2,where ω1 and ω2 stand for the first-order and second-order natural vibration frequency, respectively, and ξ for the damping ratio which is 0.02 for steel structures.


## 3.3. Defined Failure Scenarios

Three pole-legs in tripole tower are numbered as shown in Figure4(a). For wind direction Tri-A and Tri-B, the failure of leg members in pole-leg 1 is most unfavorable. For wind direction Tri-C, the failure of leg members in pole-leg 2 and 3 are both analyzed. From elevation view, the bottom leg member of each tower section is removed notionally as shown in Figure 4(b), namely, ten failure scenarios for each pole-leg.Figure 4
Positions of leg member removal at tripole tower. (a) Plan view; (b) elevation view (take section 9 and 10 for example).
(a)
(b)Figure5(a) shows the number of angle-legs and the corresponding wind direction. For wind direction Ang-A, angle-leg 1 and 2 are chosen to analyze due to the symmetrical arrangement. Angle-leg 1 and 3 would be considered in the analysis for wind direction Ang-B. Nine failure scenarios are defined for each angle-leg as shown in Figure 5(b).Figure 5
Positions of leg member removal at angle tower. (a) Plan view; (b) elevation view (take section 9 and 10 for example).
(a)
(b)


## 4. Results and Discussions

### 4.1. Tripole Tower

The horizontal displacement-time history curves of tower top whose elevation is 50 m are recorded to present the dynamic response of the tower under leg member removal in a certain tower section. According to [18], the horizontal displacement limitation for tower top in nonlinear analysis is 1/50 of the elevation. In this study, this limitation is 1 m for both tripole tower and angle tower.


#### 4.1.1. Wind Direction Tri-A

Pole-leg 1 is in compression at wind direction Tri-A. Figure6 shows the horizontal displacement-time history curves of tower top under leg member removal in pole-leg 1 at wind direction Tri-A. As Figure 6 shows, the horizontal displacement of tower top is 0.353 m after the horizontal wind loads are applied which is smaller than the limitation. For the first three tower sections, the horizontal displacement of tower top is smaller than 1 m after the leg member removed which means the tower does not collapse in these three failure scenarios. After the leg member is removed in tower section 4, the horizontal displacement of tower top spikes from 0.353 m to 2 m which is two times larger than the limitation; even then, the tower does not collapse. It suggests that the failure of the leg members in tower section 4 may have the potential to trigger the collapse of the tower. For the failure scenarios of leg members in the rest of the tower sections, the horizontal displacement of tower top tends to infinity which means that the tower would collapse.Figure 6
Leg member removal in pole-leg 1 at wind direction Tri-A.


#### 4.1.2. Wind Direction Tri-B

Pole-leg 1 is in tension at wind direction Tri-B. Figure7 shows the horizontal displacement-time history curves of tower top under leg member removal in pole-leg 1 at wind direction Tri-B. It can be seen that the failure of leg members in the first three tower sections does not cause the collapse of the tower. The failure of leg members in tower section 4 and tower section 5 would remarkably increase the horizontal displacement of tower top, yet not directly cause the collapse of the tower. For the failure scenarios in other lower tower sections, the collapse of the tower is observed. It is worth noticing that the horizontal displacement of tower top in the failure scenarios of first four tower sections is smaller than that at wind direction Tri-A. It is because the gravity load of the tower would bring about internal force in the same direction with wind loads at wind direction Tri-A. On the contrary, the gravity load of the tower would contribute to resist the collapse at wind direction Tri-B. It may be concluded that tripole tower possesses better anticollapse resistance at wind direction Tri-B than that at wind direction Tri-A.Figure 7
Leg member removal in pole-leg 1 at wind direction Tri-B.


#### 4.1.3. Wind Direction Tri-C

At wind direction Tri-C, pole-leg 2 is in compression whilst pole-leg 3 is in tension. The horizontal displacements of tower top at both down wind direction and vertical wind direction are monitored due to the torsional deformation of the tower at wind direction Tri-C.Figure8 shows the horizontal displacement-time history curves of tower top under leg member removal in pole-leg 2 at wind direction Tri-C. It can be seen that the failure of leg members in the pole-leg 2 of the first three tower sections does not cause the collapse of the tower. The vector sum of horizontal displacement of tower top in the failure scenario of tower section 4 is about 1.14 m which is a little larger than the limitation. It may be concluded that the failure scenario of tower section 4 may not initiate the collapse of the tower. The failure in the rest of the tower sections would trigger the collapse of the tower, due to the nonconvergence of horizontal displacement of tower top.Figure 8
Leg member removal in pole-leg 2 at wind direction Tri-C. (a) Down wind direction; (b) vertical wind direction.
(a)
(b)Figure9 shows the horizontal displacement-time history curves of tower top under leg member removal in pole-leg 3 at wind direction Tri-C. Comparing with pole-leg 2, the horizontal displacement of tower top in each scenario of pole-leg 3 is smaller due to the beneficial effect of gravity loads. Based on the above analysis of three wind directions, it may be concluded that the member failure of the pole-leg in compression is more unfavorable than that in tension.Figure 9
Leg member removal in pole-leg 3 at wind direction Tri-C. (a) Down wind direction; (b) vertical wind direction.
(a)
(b)


### 4.2. Angle Tower

#### 4.2.1. Wind Direction Ang-A

At wind direction Ang-A, angle-leg 1 is in tension whilst angle-leg 2 is in compression. The horizontal displacements of tower top at both down wind direction and vertical wind direction are recorded due to the torsional deformation of angle tower at wind direction Ang-A.Figures10 and 11 show the horizontal displacement-time history curves of tower top at wind direction Ang-A under leg member removal in angle-leg 1 and angle-leg 2, respectively. As they show, the horizontal displacement of tower top is 0.114 m after the horizontal wind loads are applied which is only 0.1 times of the limitation. Meanwhile, it is worth noticing that the failure of leg members in angle-leg 1 and angle-leg 2 would not trigger the collapse of angle tower. After vibrating, the horizontal displacement of tower top remains under the displacement limitation. The results show that angle tower possesses the redundancy and resistance to progressive collapse under the scenario of single member failure at wind direction Ang-A.Figure 10
Leg member removal in angle-leg 1 at wind direction Ang-A. (a) Down wind direction; (b) vertical wind direction.
(a)
(b)Figure 11
Leg member removal in angle-leg 2 at wind direction Ang-A. (a) Down wind direction; (b) vertical wind direction.
(a)
(b)


#### 4.2.2. Wind Direction Ang-B

At wind direction Ang-A, angle-leg 1 is in tension whilst angle-leg 3 is in compression. Figures12 and 13 show the horizontal displacement-time history curves of tower top at wind direction Ang-B under leg member removal in angle-leg 1 and angle-leg 3, respectively. It can be seen that the maximum horizontal displacement of tower top in the failure scenarios is about 0.325 m which is much smaller than the limitation. This shows that angle tower is also insensitive to progressive collapse under the scenario of single member failure at wind direction Ang-B.Figure 12
Leg member removal in angle-leg 1 at wind direction Ang-B.Figure 13
Leg member removal in angle-leg 3 at wind direction Ang-B.It is worth noticing that the horizontal displacement of tower top at wind direction Ang-B is larger than that at wind direction Ang-A. It is because only angle-leg 1 and angle-leg 3 are bearing the wind load at wind direction Ang-B whilst four angle-legs are all sustaining the wind load at wind direction Ang-A. It means that more internal force needs to be redistributed under the member failure at wind direction Ang-B than that at wind direction Ang-A.


### 4.3. Dynamic Sensitivity Index

Dynamic sensitivity index (DSI) as described by (5) is used in the design to assess the structural members in tower legs. Based on the horizontal displacement limitation which is 1 m [18], the corresponding limitation value DSIlim is 1.83 and 7.77 for tripole tower and angle tower, respectively. If the DSI of certain member is larger than DSIlim, the member has potential to trigger the collapse of the tower. DSIlim could be specified based on the different limitation in standards and codes.(5)DSI=Dmd−DisDis,where Dmd stands for the maximum dynamic displacement and Dis for the initial static displacement.Figure14 shows the DSIs of tripole tower and angle tower. As shown in Figure 14(a), the first three tower sections are safe in all three wind directions. The absence of DSI from tower section 6 to tower section 10 in Figure 14(a) implies the collapse of the tower. The DSI of pole-leg 2 in tower section 4 and pole-leg 3 in tower section 5 at wind direction Tri-C is only 1.1 times higher than the limitation value DSIlim. Comparing the DSIs of different wind directions, it could be concluded that wind direction Tri-A that causes single pole-leg in compression is the most unfavorable wind direction for tripole tower. As shown in Figure 14(b), the DSIs of angle tower are much lower than the limitation value which suggests that there is no potential to collapse in angle tower under the scenario of single angle-leg failure. Still, it can be seen in Figure 14(b) that wind direction Ang-B is the most unfavorable wind direction for angle tower.Figure 14
DSI of the towers. (a) Tripole tower; (b) angle tower.
(a)
(b)


### 4.4. Collapse Probability

Based on the research in [19], the collapse probability of telecommunication tower under wind loads P[C] can be expressed as(6)PC=PCLW·PL·PW,where P[W]  is the  probability of most unfavorable wind direction, P[L]  is the  probability of leg member failure, and P[C/LW]  is the  probability of collapse under the occurrence of both most unfavorable wind direction and leg member failure.The collapse probabilityP[C] should be limited to a certain value that is acceptable to the society. However, so far there is no specific standard value proposed by researchers or in standards. Still risk management should be adopted to minimize the probability of the three terms in (6). To this end, three different levels of anticollapse strategies should be adopted in the design and renewal of latticed telecommunication towers: (a) to avoid the most unfavorable wind direction through proper design; (b) to protect or enhance the critical leg member that has potential to trigger a collapse; and (c) to prevent tower collapse through anticollapse design, such as alternative load path or bridge over method.Note thatP[W] and P[L] actually are two irrelevant variables. P[W] could be predicted by the statistics of local prevailing wind range and wind rose diagram. P[L] is hard to be predicted, for the leg member failure may be caused by vandalism, rather than wind load. According to GSA and DoD, the members in lower elevation are more vulnerable than those in higher elevation. Therefore, a relative value of P[L] based on member elevation could be used in the assessment of P[C], as shown in Figure 15.Figure 15
Probability of leg member failure.In alternative load path method, the aim is to control the probabilityP[C/LW], which is to minimize the propagation of initial failure. The probability P[C/LW] could be calculated as(7)PCLW=ncn,where nc and n stand for the number of the collapse scenarios and that of all the failure scenarios, respectively.Based on the aforementioned analysis, the probabilityP[C/LW] of tripole tower under design wind load referring to elevation which is calculated by (7) is illustrated in Figure 16. Lognormal distribution function [20] is adopted to fit the probability P[C/LW] of tripole tower under design wind load referring to elevation. As shown in Figure 16, the collapse probability of tripole tower under the occurrence of both most unfavorable wind direction and leg member failure follows a lognormal distribution. More study in the future should be focused on the probability P[C/LW] of various types of tripole tower.Figure 16
P[C/LW] of tripole tower under design wind load referring to elevation.If all representative unfavorable wind directions and member failure scenarios are taken into account in the analysis, it can be assumed thatP[W]P[L] = 1 and that only the conditional probability P[C/LW], namely, the collapse probability under certain level of wind load after initial failure, is adopted to assess the potential to progressive collapse of latticed towers. Therefore, the collapse probability P[C] of 50 m high tripole tower under design wind load can be calculated as(8)PC=ncn=0.625.The collapse probability of 50 m high angle tower under design wind load is zero which means the robustness of this tower is enough to resist progressive collapse under design wind load.In order to assess the collapse probability of the latticed towers under different normalized wind loads, 10 nominal wind levels are applied at 50 m high tripole tower and 50 m high angle tower. Aforementioned design wind load is defined as 1.0 W. The progressive collapse fragile curves of the towers could be established as shown in Figure17, which can also be described by the lognormal distribution function. The vertical axis in Figure 17 is the collapse probability in (6), whilst the horizontal axis is the nominal wind load, namely, intensity measure (IM).Figure 17
Progressive collapse fragile curves of the towers.When IM = 1.0 W (W is the design wind load), the corresponding value is the collapse probability under design wind load, which is 0.625 for tripole tower and zero for angle tower. It suggests that angle tower completely meets the anticollapse demand, even though anticollapse design is normally not considered in the design of the tower. The collapse probability of robust latticed tower is supposed to be zero in any scenarios of expected member failure under design wind load (P[C] = 0 when IM ≦ 1.0 W).In the anticollapse design of latticed tower, progressive collapse fragile curve should be used to assess the anticollapse performance of the tower as follows:(1)
Establish a numerical model of the overall latticed tower, chose one or several unfavorable wind direction, and conduct a dynamic analysis of member removal(2)
Repeat step 1 for all representative removal scenarios under certain nominal wind load and calculate the collapse probability(3)
Continuously change the nominal wind load and repeat step 1–2 to obtain a series of collapse probability under nominal wind load, and plot the progressive collapse fragile curve(4)
Considering the construction cost and safety of the tower, decide the acceptable collapse probability of the tower under certain wind load level(5)
Change the design of the tower and repeat step 1–4 to obtain an acceptable progressive collapse fragile curve (more vulnerable but cheaper cost or more robust but expensive cost) as shown in Figure18Figure 18
Anticollapse design.As shown in Figure18, various progressive collapse fragile curves are obtained by changing the design of the tower. Normal P[C] corresponds to design wind load on the tower. By enhancing the tower, the curve would shift toward right which means the collapse probability decreases under each level of wind loads. On the contrary, the curve would shift toward left by weakening the tower, which means the collapse probability increases under each level of wind loads, but the construction cost of tower would decrease.


## 4.1. Tripole Tower

The horizontal displacement-time history curves of tower top whose elevation is 50 m are recorded to present the dynamic response of the tower under leg member removal in a certain tower section. According to [18], the horizontal displacement limitation for tower top in nonlinear analysis is 1/50 of the elevation. In this study, this limitation is 1 m for both tripole tower and angle tower.


### 4.1.1. Wind Direction Tri-A

Pole-leg 1 is in compression at wind direction Tri-A. Figure6 shows the horizontal displacement-time history curves of tower top under leg member removal in pole-leg 1 at wind direction Tri-A. As Figure 6 shows, the horizontal displacement of tower top is 0.353 m after the horizontal wind loads are applied which is smaller than the limitation. For the first three tower sections, the horizontal displacement of tower top is smaller than 1 m after the leg member removed which means the tower does not collapse in these three failure scenarios. After the leg member is removed in tower section 4, the horizontal displacement of tower top spikes from 0.353 m to 2 m which is two times larger than the limitation; even then, the tower does not collapse. It suggests that the failure of the leg members in tower section 4 may have the potential to trigger the collapse of the tower. For the failure scenarios of leg members in the rest of the tower sections, the horizontal displacement of tower top tends to infinity which means that the tower would collapse.Figure 6
Leg member removal in pole-leg 1 at wind direction Tri-A.


### 4.1.2. Wind Direction Tri-B

Pole-leg 1 is in tension at wind direction Tri-B. Figure7 shows the horizontal displacement-time history curves of tower top under leg member removal in pole-leg 1 at wind direction Tri-B. It can be seen that the failure of leg members in the first three tower sections does not cause the collapse of the tower. The failure of leg members in tower section 4 and tower section 5 would remarkably increase the horizontal displacement of tower top, yet not directly cause the collapse of the tower. For the failure scenarios in other lower tower sections, the collapse of the tower is observed. It is worth noticing that the horizontal displacement of tower top in the failure scenarios of first four tower sections is smaller than that at wind direction Tri-A. It is because the gravity load of the tower would bring about internal force in the same direction with wind loads at wind direction Tri-A. On the contrary, the gravity load of the tower would contribute to resist the collapse at wind direction Tri-B. It may be concluded that tripole tower possesses better anticollapse resistance at wind direction Tri-B than that at wind direction Tri-A.Figure 7
Leg member removal in pole-leg 1 at wind direction Tri-B.


### 4.1.3. Wind Direction Tri-C

At wind direction Tri-C, pole-leg 2 is in compression whilst pole-leg 3 is in tension. The horizontal displacements of tower top at both down wind direction and vertical wind direction are monitored due to the torsional deformation of the tower at wind direction Tri-C.Figure8 shows the horizontal displacement-time history curves of tower top under leg member removal in pole-leg 2 at wind direction Tri-C. It can be seen that the failure of leg members in the pole-leg 2 of the first three tower sections does not cause the collapse of the tower. The vector sum of horizontal displacement of tower top in the failure scenario of tower section 4 is about 1.14 m which is a little larger than the limitation. It may be concluded that the failure scenario of tower section 4 may not initiate the collapse of the tower. The failure in the rest of the tower sections would trigger the collapse of the tower, due to the nonconvergence of horizontal displacement of tower top.Figure 8
Leg member removal in pole-leg 2 at wind direction Tri-C. (a) Down wind direction; (b) vertical wind direction.
(a)
(b)Figure9 shows the horizontal displacement-time history curves of tower top under leg member removal in pole-leg 3 at wind direction Tri-C. Comparing with pole-leg 2, the horizontal displacement of tower top in each scenario of pole-leg 3 is smaller due to the beneficial effect of gravity loads. Based on the above analysis of three wind directions, it may be concluded that the member failure of the pole-leg in compression is more unfavorable than that in tension.Figure 9
Leg member removal in pole-leg 3 at wind direction Tri-C. (a) Down wind direction; (b) vertical wind direction.
(a)
(b)


## 4.1.1. Wind Direction Tri-A

Pole-leg 1 is in compression at wind direction Tri-A. Figure6 shows the horizontal displacement-time history curves of tower top under leg member removal in pole-leg 1 at wind direction Tri-A. As Figure 6 shows, the horizontal displacement of tower top is 0.353 m after the horizontal wind loads are applied which is smaller than the limitation. For the first three tower sections, the horizontal displacement of tower top is smaller than 1 m after the leg member removed which means the tower does not collapse in these three failure scenarios. After the leg member is removed in tower section 4, the horizontal displacement of tower top spikes from 0.353 m to 2 m which is two times larger than the limitation; even then, the tower does not collapse. It suggests that the failure of the leg members in tower section 4 may have the potential to trigger the collapse of the tower. For the failure scenarios of leg members in the rest of the tower sections, the horizontal displacement of tower top tends to infinity which means that the tower would collapse.Figure 6
Leg member removal in pole-leg 1 at wind direction Tri-A.


## 4.1.2. Wind Direction Tri-B

Pole-leg 1 is in tension at wind direction Tri-B. Figure7 shows the horizontal displacement-time history curves of tower top under leg member removal in pole-leg 1 at wind direction Tri-B. It can be seen that the failure of leg members in the first three tower sections does not cause the collapse of the tower. The failure of leg members in tower section 4 and tower section 5 would remarkably increase the horizontal displacement of tower top, yet not directly cause the collapse of the tower. For the failure scenarios in other lower tower sections, the collapse of the tower is observed. It is worth noticing that the horizontal displacement of tower top in the failure scenarios of first four tower sections is smaller than that at wind direction Tri-A. It is because the gravity load of the tower would bring about internal force in the same direction with wind loads at wind direction Tri-A. On the contrary, the gravity load of the tower would contribute to resist the collapse at wind direction Tri-B. It may be concluded that tripole tower possesses better anticollapse resistance at wind direction Tri-B than that at wind direction Tri-A.Figure 7
Leg member removal in pole-leg 1 at wind direction Tri-B.


## 4.1.3. Wind Direction Tri-C

At wind direction Tri-C, pole-leg 2 is in compression whilst pole-leg 3 is in tension. The horizontal displacements of tower top at both down wind direction and vertical wind direction are monitored due to the torsional deformation of the tower at wind direction Tri-C.Figure8 shows the horizontal displacement-time history curves of tower top under leg member removal in pole-leg 2 at wind direction Tri-C. It can be seen that the failure of leg members in the pole-leg 2 of the first three tower sections does not cause the collapse of the tower. The vector sum of horizontal displacement of tower top in the failure scenario of tower section 4 is about 1.14 m which is a little larger than the limitation. It may be concluded that the failure scenario of tower section 4 may not initiate the collapse of the tower. The failure in the rest of the tower sections would trigger the collapse of the tower, due to the nonconvergence of horizontal displacement of tower top.Figure 8
Leg member removal in pole-leg 2 at wind direction Tri-C. (a) Down wind direction; (b) vertical wind direction.
(a)
(b)Figure9 shows the horizontal displacement-time history curves of tower top under leg member removal in pole-leg 3 at wind direction Tri-C. Comparing with pole-leg 2, the horizontal displacement of tower top in each scenario of pole-leg 3 is smaller due to the beneficial effect of gravity loads. Based on the above analysis of three wind directions, it may be concluded that the member failure of the pole-leg in compression is more unfavorable than that in tension.Figure 9
Leg member removal in pole-leg 3 at wind direction Tri-C. (a) Down wind direction; (b) vertical wind direction.
(a)
(b)


## 4.2. Angle Tower

### 4.2.1. Wind Direction Ang-A

At wind direction Ang-A, angle-leg 1 is in tension whilst angle-leg 2 is in compression. The horizontal displacements of tower top at both down wind direction and vertical wind direction are recorded due to the torsional deformation of angle tower at wind direction Ang-A.Figures10 and 11 show the horizontal displacement-time history curves of tower top at wind direction Ang-A under leg member removal in angle-leg 1 and angle-leg 2, respectively. As they show, the horizontal displacement of tower top is 0.114 m after the horizontal wind loads are applied which is only 0.1 times of the limitation. Meanwhile, it is worth noticing that the failure of leg members in angle-leg 1 and angle-leg 2 would not trigger the collapse of angle tower. After vibrating, the horizontal displacement of tower top remains under the displacement limitation. The results show that angle tower possesses the redundancy and resistance to progressive collapse under the scenario of single member failure at wind direction Ang-A.Figure 10
Leg member removal in angle-leg 1 at wind direction Ang-A. (a) Down wind direction; (b) vertical wind direction.
(a)
(b)Figure 11
Leg member removal in angle-leg 2 at wind direction Ang-A. (a) Down wind direction; (b) vertical wind direction.
(a)
(b)


### 4.2.2. Wind Direction Ang-B

At wind direction Ang-A, angle-leg 1 is in tension whilst angle-leg 3 is in compression. Figures12 and 13 show the horizontal displacement-time history curves of tower top at wind direction Ang-B under leg member removal in angle-leg 1 and angle-leg 3, respectively. It can be seen that the maximum horizontal displacement of tower top in the failure scenarios is about 0.325 m which is much smaller than the limitation. This shows that angle tower is also insensitive to progressive collapse under the scenario of single member failure at wind direction Ang-B.Figure 12
Leg member removal in angle-leg 1 at wind direction Ang-B.Figure 13
Leg member removal in angle-leg 3 at wind direction Ang-B.It is worth noticing that the horizontal displacement of tower top at wind direction Ang-B is larger than that at wind direction Ang-A. It is because only angle-leg 1 and angle-leg 3 are bearing the wind load at wind direction Ang-B whilst four angle-legs are all sustaining the wind load at wind direction Ang-A. It means that more internal force needs to be redistributed under the member failure at wind direction Ang-B than that at wind direction Ang-A.


## 4.2.1. Wind Direction Ang-A

At wind direction Ang-A, angle-leg 1 is in tension whilst angle-leg 2 is in compression. The horizontal displacements of tower top at both down wind direction and vertical wind direction are recorded due to the torsional deformation of angle tower at wind direction Ang-A.Figures10 and 11 show the horizontal displacement-time history curves of tower top at wind direction Ang-A under leg member removal in angle-leg 1 and angle-leg 2, respectively. As they show, the horizontal displacement of tower top is 0.114 m after the horizontal wind loads are applied which is only 0.1 times of the limitation. Meanwhile, it is worth noticing that the failure of leg members in angle-leg 1 and angle-leg 2 would not trigger the collapse of angle tower. After vibrating, the horizontal displacement of tower top remains under the displacement limitation. The results show that angle tower possesses the redundancy and resistance to progressive collapse under the scenario of single member failure at wind direction Ang-A.Figure 10
Leg member removal in angle-leg 1 at wind direction Ang-A. (a) Down wind direction; (b) vertical wind direction.
(a)
(b)Figure 11
Leg member removal in angle-leg 2 at wind direction Ang-A. (a) Down wind direction; (b) vertical wind direction.
(a)
(b)


## 4.2.2. Wind Direction Ang-B

At wind direction Ang-A, angle-leg 1 is in tension whilst angle-leg 3 is in compression. Figures12 and 13 show the horizontal displacement-time history curves of tower top at wind direction Ang-B under leg member removal in angle-leg 1 and angle-leg 3, respectively. It can be seen that the maximum horizontal displacement of tower top in the failure scenarios is about 0.325 m which is much smaller than the limitation. This shows that angle tower is also insensitive to progressive collapse under the scenario of single member failure at wind direction Ang-B.Figure 12
Leg member removal in angle-leg 1 at wind direction Ang-B.Figure 13
Leg member removal in angle-leg 3 at wind direction Ang-B.It is worth noticing that the horizontal displacement of tower top at wind direction Ang-B is larger than that at wind direction Ang-A. It is because only angle-leg 1 and angle-leg 3 are bearing the wind load at wind direction Ang-B whilst four angle-legs are all sustaining the wind load at wind direction Ang-A. It means that more internal force needs to be redistributed under the member failure at wind direction Ang-B than that at wind direction Ang-A.


## 4.3. Dynamic Sensitivity Index

Dynamic sensitivity index (DSI) as described by (5) is used in the design to assess the structural members in tower legs. Based on the horizontal displacement limitation which is 1 m [18], the corresponding limitation value DSIlim is 1.83 and 7.77 for tripole tower and angle tower, respectively. If the DSI of certain member is larger than DSIlim, the member has potential to trigger the collapse of the tower. DSIlim could be specified based on the different limitation in standards and codes.(5)DSI=Dmd−DisDis,where Dmd stands for the maximum dynamic displacement and Dis for the initial static displacement.Figure14 shows the DSIs of tripole tower and angle tower. As shown in Figure 14(a), the first three tower sections are safe in all three wind directions. The absence of DSI from tower section 6 to tower section 10 in Figure 14(a) implies the collapse of the tower. The DSI of pole-leg 2 in tower section 4 and pole-leg 3 in tower section 5 at wind direction Tri-C is only 1.1 times higher than the limitation value DSIlim. Comparing the DSIs of different wind directions, it could be concluded that wind direction Tri-A that causes single pole-leg in compression is the most unfavorable wind direction for tripole tower. As shown in Figure 14(b), the DSIs of angle tower are much lower than the limitation value which suggests that there is no potential to collapse in angle tower under the scenario of single angle-leg failure. Still, it can be seen in Figure 14(b) that wind direction Ang-B is the most unfavorable wind direction for angle tower.Figure 14
DSI of the towers. (a) Tripole tower; (b) angle tower.
(a)
(b)


## 4.4. Collapse Probability

Based on the research in [19], the collapse probability of telecommunication tower under wind loads P[C] can be expressed as(6)PC=PCLW·PL·PW,where P[W]  is the  probability of most unfavorable wind direction, P[L]  is the  probability of leg member failure, and P[C/LW]  is the  probability of collapse under the occurrence of both most unfavorable wind direction and leg member failure.The collapse probabilityP[C] should be limited to a certain value that is acceptable to the society. However, so far there is no specific standard value proposed by researchers or in standards. Still risk management should be adopted to minimize the probability of the three terms in (6). To this end, three different levels of anticollapse strategies should be adopted in the design and renewal of latticed telecommunication towers: (a) to avoid the most unfavorable wind direction through proper design; (b) to protect or enhance the critical leg member that has potential to trigger a collapse; and (c) to prevent tower collapse through anticollapse design, such as alternative load path or bridge over method.Note thatP[W] and P[L] actually are two irrelevant variables. P[W] could be predicted by the statistics of local prevailing wind range and wind rose diagram. P[L] is hard to be predicted, for the leg member failure may be caused by vandalism, rather than wind load. According to GSA and DoD, the members in lower elevation are more vulnerable than those in higher elevation. Therefore, a relative value of P[L] based on member elevation could be used in the assessment of P[C], as shown in Figure 15.Figure 15
Probability of leg member failure.In alternative load path method, the aim is to control the probabilityP[C/LW], which is to minimize the propagation of initial failure. The probability P[C/LW] could be calculated as(7)PCLW=ncn,where nc and n stand for the number of the collapse scenarios and that of all the failure scenarios, respectively.Based on the aforementioned analysis, the probabilityP[C/LW] of tripole tower under design wind load referring to elevation which is calculated by (7) is illustrated in Figure 16. Lognormal distribution function [20] is adopted to fit the probability P[C/LW] of tripole tower under design wind load referring to elevation. As shown in Figure 16, the collapse probability of tripole tower under the occurrence of both most unfavorable wind direction and leg member failure follows a lognormal distribution. More study in the future should be focused on the probability P[C/LW] of various types of tripole tower.Figure 16
P[C/LW] of tripole tower under design wind load referring to elevation.If all representative unfavorable wind directions and member failure scenarios are taken into account in the analysis, it can be assumed thatP[W]P[L] = 1 and that only the conditional probability P[C/LW], namely, the collapse probability under certain level of wind load after initial failure, is adopted to assess the potential to progressive collapse of latticed towers. Therefore, the collapse probability P[C] of 50 m high tripole tower under design wind load can be calculated as(8)PC=ncn=0.625.The collapse probability of 50 m high angle tower under design wind load is zero which means the robustness of this tower is enough to resist progressive collapse under design wind load.In order to assess the collapse probability of the latticed towers under different normalized wind loads, 10 nominal wind levels are applied at 50 m high tripole tower and 50 m high angle tower. Aforementioned design wind load is defined as 1.0 W. The progressive collapse fragile curves of the towers could be established as shown in Figure17, which can also be described by the lognormal distribution function. The vertical axis in Figure 17 is the collapse probability in (6), whilst the horizontal axis is the nominal wind load, namely, intensity measure (IM).Figure 17
Progressive collapse fragile curves of the towers.When IM = 1.0 W (W is the design wind load), the corresponding value is the collapse probability under design wind load, which is 0.625 for tripole tower and zero for angle tower. It suggests that angle tower completely meets the anticollapse demand, even though anticollapse design is normally not considered in the design of the tower. The collapse probability of robust latticed tower is supposed to be zero in any scenarios of expected member failure under design wind load (P[C] = 0 when IM ≦ 1.0 W).In the anticollapse design of latticed tower, progressive collapse fragile curve should be used to assess the anticollapse performance of the tower as follows:(1)
Establish a numerical model of the overall latticed tower, chose one or several unfavorable wind direction, and conduct a dynamic analysis of member removal(2)
Repeat step 1 for all representative removal scenarios under certain nominal wind load and calculate the collapse probability(3)
Continuously change the nominal wind load and repeat step 1–2 to obtain a series of collapse probability under nominal wind load, and plot the progressive collapse fragile curve(4)
Considering the construction cost and safety of the tower, decide the acceptable collapse probability of the tower under certain wind load level(5)
Change the design of the tower and repeat step 1–4 to obtain an acceptable progressive collapse fragile curve (more vulnerable but cheaper cost or more robust but expensive cost) as shown in Figure18Figure 18
Anticollapse design.As shown in Figure18, various progressive collapse fragile curves are obtained by changing the design of the tower. Normal P[C] corresponds to design wind load on the tower. By enhancing the tower, the curve would shift toward right which means the collapse probability decreases under each level of wind loads. On the contrary, the curve would shift toward left by weakening the tower, which means the collapse probability increases under each level of wind loads, but the construction cost of tower would decrease.


## 5. Conclusions

In this paper, nonlinear dynamic analysis is conducted on typical standard latticed telecommunication tripole tower and angle tower by alternative load path method. The finite element models for two towers subjected to design wind loads are developed by ABAQUS. The following conclusions are made:(1)
For 50 m high standard tripole tower, the member failure in the first three tower sections from tower top would not trigger the collapse of the tower. From the fourth tower section to tower bottom, the member failure at certain wind direction may cause a collapse. Wind direction Tri-A that causes single pole-leg in compression is the most unfavorable wind direction for tripole tower.(2)
For 50 m high standard angle tower, the single member failure in any tower section would not cause the collapse of the tower. Wind direction Ang-B is the most unfavorable wind direction for angle tower.(3)
A progressive collapse fragile curve based on collapse probability of telecommunication tower under wind loads is proposed to assess the anticollapse performance of the towers.



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*Source: 3293506-2018-01-24.xml*