3.1. Stress Distribution Model Under Individual Headed Bars
The stress distribution model is analyzed using a cube model. The size of the model is 2
h × 2
h × 2
h, and the side length of the headed bars is 2
a. When the model is subjected to local compression, the stress under the headed bars diffuses some distance before it can be diffused to the full cross-section. During this diffusion process, the local compression-affected area of concrete under the headed bars forms a compression region and a tensile region. The height of the compression region is the side length of the headed bars 2
a. The tensile region is the stress diffused to the full cross-section of the specimen in the form of an umbrella, and the height of the tensile region is 2
h − 2
a. The stress distribution of the local compression of model is shown in
Figure 4. The distribution form of the outermost stress curve in the tensile region of the specimen is simplified into a quadratic parabola, which is expressed in a Cartesian coordinate system, as shown in
Figure 5.
From coordinates (
a, 2
h − 2
a), (
h, 0), the equation of the stress curve can be obtained as
When the stress of the model diffuses to the full cross-section under local compression
NP, the full cross-section area is the concrete area for distributing the bearing. So,
h is 3
a. By further simplifying Equation (1), the stress curve equation is obtained as follows:
According to Equation (2), each cross-section side length of the model 2
x can be obtained as follows:
The model size is 2
h × 2
h × 2
h, that is, the stress is diffused to each cross-section of the model in a square cross-section with a side length of 2
x. Therefore, the stress distribution area of each cross-section of the model is 4
x2. According to Equation (3), the cross-section area under individual headed bars of the model
A1 is as follows:
Considering that the local compression cannot decay during the load process, the local compression applied to each cross-section of the model is consistent. Therefore, the expression of the average stress of each cross-section in the tensile region of the model
σt,avg is
Under local compression
NP, the stress diffuses in the compression region in the form of straight lines, that is, each cross-section area in the compression region of the model is equal, and each cross-section area is 4
a2. The local compression
NP cannot decay during the load process; that is, the
NP applied to each cross-section of the model is consistent. Therefore, the expression of the average stress of each cross-section in the compression region of the model
σc,avg is
According to Equations (5) and (6), the average stress of each cross-section in the compression region and the tensile region of the model can be obtained under local compression
NP. The stress curve in different cross-sections of the model can be obtained. The stress curve is shown in
Figure 6.
According to the stress curves in different cross-sections, as shown in
Figure 6, the
σc,avg in the compression region of the model is equal, while the
σt,avg in the tensile region of the model gradually weakens as the stress diffuses to the full cross-section. The stress variation rate reflects the stress variation trend of each cross-section. The
σt,avg has a large change trend in the initial transfer process of the tensile region, and the curve change amplitude is large. As the stress continues to diffuse downward along the tensile region of the model, the
σt,avg changes less, and the curve changes the amplitude less. When the stress is about to diffuse to the full cross-section, the change trend of the
σt,avg is minimal, and the change amplitude of the curve tends to remain unchanged. When
y = 0, the stress of the full cross-section
σ0 can be obtained from Equation (5). Take the height of the smaller distance from the full cross-section as
y1, and the
σy1 can be obtained using Equation (5). Then, the stress variation rate δ
1 that stress is about to diffuse to the full cross-section is
3.2. Stress Distribution Model Under Two Headed Bars
Similarly to individual headed bars, when two headed bars are jointly stressed, the stress first diffuses in the compression region of the model, and then it diffuses in the tensile region in the form of an umbrella until the full cross-section. When c is twice or more than twice the side length of the headed bars, the stress under two headed bars cannot overlap; therefore, the σt,avg of each cross-section in the tensile region is not affected. At this time, the stress under two headed bars of the model is considered according to the stress under individual headed bars. When c is greater than 0 mm but less than twice the side length of the headed bars, the overlapped area of stress under two headed bars decreases from the maximum with the increase in the c. Due to the influence of overlapping stress under two headed bars, the σt,avg of each cross-section in the tensile region under two headed bars will be larger than the σt,avg under individual headed bars. In this case, the stress of different cross-sections under two headed bars will be formed, and the change trend of σt,avg and σc,avg will be formed. The stress under two headed bars is also a process of diffusion to the full cross-section. Different to individual headed bars, the stress change trend of σt,avg keeps a relatively long distance unchanged in the tensile region when stress diffuses to the full cross-section under two headed bars. So, it is considered that the stress has diffused to the full cross-section in advance. The stress diffused to the full cross-section when the stress variation trend is under two headed bars is equal to the stress variation trend under individual headed bars. That is, the stress variation rate under two headed bars is the same as the stress variation rate δ1 under individual headed bars.
The size of the model is 4
h × 2
h, and the height is 4
h. The headed bars are square, and the side length is 2
a. Under local compression 2
NP, the stress first diffuses 2
a in the compression region and then diffuses to the tensile region in the form of an umbrella. The model is shown in
Figure 7.
It can be seen from
Figure 7 each cross-section area in the tensile region of the model in the process of local compression. Each cross-section area is composed of the distance between the outermost curves of stress under two headed bars and individual headed bars. The distance between the outermost curves of the stress under individual headed bars is 2
x. The distance between the outermost curves of stress under two headed bars is the sum of the distance between the outermost curves of stress under individual headed bars and the side length of the headed bars and
c. That is, 2
x + 2
a +
c. Therefore, the stress distribution area of each cross-section of the model is 4
x2 + 4
ax + 2
cx. It can be concluded that each cross-section area of the model
A2 is
Under local compression 2
NP, the 2
NP applied to each cross-section of the model is consistent. The expression of
σt,avg of each cross-section in tensile region of the model is
Due to the influence of overlapping stress under two headed bars, the stress diffuses to the full cross-section earlier. According to Equation (9), the stress of each cross-section in the tensile region of the model
σt,avg can be obtained under local compression 2
NP, and the stress of each cross-section in the compression region of the model
σc,avg is equal to
σc,avg under individual headed bars. The stress curve in different cross-sections of the model can be obtained. The height of stress diffused to the full cross-section under two headed bars is set as
y2, and the height
y3 is taken as the shorter distance from the
y2. The stress curve is shown in
Figure 8. The stress variation rate δ
2 is
According to Equations (7) and (10), the expression of the stress variation rate δ
2 under two headed bars, which is consistent with the stress variation rate δ
1 under individual headed bars when the stress is about to diffuse to the full cross-section, can be obtained as follows:
When the stress is about to diffuse to the full cross-section under individual headed bars, the distance from the full cross-section is shorter, and the height is
y1. When the stress is under two headed bars, the distance between two cross-sections can be determined as
y1, and then
y3 =
y2 +
y1. The modified Equation (11) can be obtained as follows:
According to Equation (12), the height of stress diffusion under two headed bars to the full cross-section
y2 can be calculated so as to determine the height of the tensile region of the model. When
c = 0, two headed bars are fitted together, and the height of the tensile region of the model can be determined based on individual headed bars. The size of the headed bars is 4
a × 2
a. Under local compression, the height of the compression region is 2
a, and the height of the tensile region is 6
a. When
c is greater than 0, the height of the tensile region
ht is defined as the different value between the height of the tensile region when
c = 0 and the height of stress diffusion under two headed bars to the full cross-section
y2, that is, 6
a−
y2. Take the distance between the two cross-sections
y1 as 1 mm, and calculate the height of the tensile region
ht of each specimen in this test according to Equation (12), as shown in
Table 5.