1. C-Shaped Core Wall Biaxial Strength Calculations

The following three figures display the section’s strain diagram, internal forces and the corresponding moment arms in the necessary nomenclature to prepare for the strength calculations of each of the following:

Design Axial Strength (φPn)

Figure 3 shows the strain diagram for the reinforcement and concrete based on the neutral axis location and angle values provided. The internal forces for the reinforcement and concrete compression block are calculated based on the strain values. φ is calculated based on the strain in the extreme tension reinforcement layer.

Design Flexural Strength (φMnx)

The flexural strength φMnx can be calculated using force values and moment arms from the x-axis (ry) as shown in Figure 4.

Design Flexural Strength (φMny)

The flexural strength φMny can be calculated using force values and moment arms from the y-axis (rx) as shown in Figure 5.

05

Figure 3 - Design Axial Strength (φPn) Calculations

06

Figure 4 - Design Flexural Strength (φMnx) Calculations

07

Figure 5 - Design Flexural Strength (φMny) Calculations

1.1. Neutral Axis Location and Concrete Compression Force

The trial-and-error process for calculating the neutral axis depth and angle α is not required in this example since these values are given (c = 36.12 in. and α = 120o)   . Where c is the distance from the fiber of maximum compressive strain to the neutral axis and α is the angle of the neutral axis.     ACI 318-19 (22.2.2.4.2)




    ACI 318-19 (Table 21.2.2)

    ACI 318-19 (22.2.2.4.1)

    ACI 318-19 (22.2.2.1)

Where:

a = Depth of equivalent rectangular stress block

    ACI 318-19 (Table 22.2.2.4.3)

   (Compression) ACI 318-19 (22.2.2.4.1)

Calculate the area of the section subject to compression and its centroid by examining the four sub segments as shown in the following figure:

















Note that and are the coordinates of the centroid of the entire cross-section (uncracked core wall section).

08

Figure 6 - Cracked Concrete Wall Section Centroid Calculations

1.2. Determination of Reinforcement Strains and Forces

The following shows the calculations of forces in the reinforcement layers with the extreme tension (at bar 1) and extreme compression (at bar 29) strains. The calculations for the rest of layers are shown the table at the end of this section.

For extreme tension reinforcement layer (at bar 1):



(Tension)

For extreme compression reinforcement layer (at bar 29):



The area of the reinforcement in this layer is included in the area used to compute Cc (a = 30.70 in. > d29 = 5.40 in.). As a result, it is necessary to subtract 0.85fc from fs29 before computing Fs29:

(Compression)

The same procedure shown above can be repeated to calculate the forces in the remaining reinforcement locations, results are summarized in the table shown in the next page:

1.3. Calculation of Pn, Mnx and Mny


(+) = Compression

(-) = Tension





(+) = Counter Clockwise

(-) = Clockwise





(+) = Counter Clockwise

(-) = Clockwise






Table 1 - Strains, internal force resultants and Moments

Location

d, in

ε, in./in.

fs, psi

Fs, kip

Cc, kip

rx, in.

My, kip-ft

ry, in.

Mx, kip-ft

Concrete

---

0.00300

---

---

2166.2

14.8

2671.6

104.0

18778.4

Bar 1

201.56

-0.01374

-60000.0

-18.6

---

-68.0

105.4

-120.0

186.0

Bar 2

190.67

-0.01284

-60000.0

-18.6

---

-55.4

85.9

-120.0

186.0

Bar 3

179.78

-0.01193

-60000.0

-18.6

---

-42.9

66.4

-120.0

186.0

Bar 4

168.89

-0.01103

-60000.0

-18.6

---

-30.3

46.9

-120.0

186.0

Bar 5

158.00

-0.01012

-60000.0

-18.6

---

-17.7

27.5

-120.0

186.0

Bar 6

147.11

-0.00922

-60000.0

-18.6

---

-5.2

8.0

-120.0

186.0

Bar 7

136.23

-0.00831

-60000.0

-18.6

---

7.4

-11.5

-120.0

186.0

Bar 8

125.34

-0.00741

-60000.0

-18.6

---

20.0

-31.0

-120.0

186.0

Bar 9

119.62

-0.00694

-60000.0

-18.6

---

20.0

-31.0

-108.6

168.3

Bar 10

113.91

-0.00646

-60000.0

-18.6

---

20.0

-31.0

-97.1

150.6

Bar 11

108.20

-0.00599

-60000.0

-18.6

---

20.0

-31.0

-84.7

131.3

Bar 12

102.49

-0.00551

-60000.0

-18.6

---

20.0

-31.0

-74.3

115.1

Bar 13

96.78

-0.00504

-60000.0

-18.6

---

20.0

-31.0

-63.2

98.0

Bar 14

91.07

-0.00456

-60000.0

-18.6

---

20.0

-31.0

-51.4

79.7

Bar 15

85.36

-0.00409

-60000.0

-18.6

---

20.0

-31.0

-40.0

62.0

Bar 16

79.65

-0.00362

-60000.0

-18.6

---

20.0

-31.0

-28.6

44.3

Bar 17

73.93

-0.00314

-60000.0

-18.6

---

20.0

-31.0

-17.1

26.6

Bar 18

68.22

-0.00267

-60000.0

-18.6

---

20.0

-31.0

-5.7

8.9

Bar 19

62.51

-0.00219

-60000.0

-18.6

---

20.0

-31.0

5.7

-8.9

Bar 20

56.80

-0.00172

-49810.6

-15.4

---

20.0

-25.7

17.1

-22.1

Bar 21

51.09

-0.00124

-36057.3

-11.2

---

20.0

-18.6

28.6

-26.6

Bar 22

45.38

-0.00077

-22304.0

-6.9

---

20.0

-11.5

40.0

-23.0

Bar 23

39.67

-0.00029

-8550.7

-2.7

---

20.0

-4.4

51.4

-11.4

Bar 24

33.95

0.00018

5226.7

1.6

---

20.0

2.7

62.9

8.5

Bar 25*

28.24

0.00065

18980.0

4.8

---

20.0

8.1

74.3

29.9

Bar 26*

22.53

0.00113

32733.4

9.1

---

20.0

15.2

85.7

64.9

Bar 27*

16.82

0.00160

46486.7

13.4

---

20.0

22.3

97.1

108.1

Bar 28*

11.11

0.00208

60000.0

17.6

---

20.0

29.3

108.6

158.8

Bar 29*

5.40

0.00255

60000.0

17.6

---

20.0

29.3

120.0

175.5

Bar 30*

16.29

0.00165

47763.3

13.8

---

7.4

8.5

120.0

137.5

Bar 31*

27.18

0.00074

21533.2

5.6

---

-5.2

-2.4

120.0

56.2

Bar 32

38.07

-0.00016

-4696.8

-1.5

---

-17.7

2.2

120.0

-14.9

Bar 33

48.95

-0.00107

-30902.8

-9.6

---

-30.3

24.2

120.0

-95.8

Bar 34

59.84

-0.00197

-57132.9

-17.7

---

-42.9

63.3

120.0

-177.1

Bar 35

70.73

-0.00287

-60000.0

-18.6

---

-55.4

85.9

120.0

-186.0

Bar 36

81.62

-0.00378

-60000.0

-18.6

---

-68.0

105.4

120.0

-186.0

Axial Force and Bending Moment Capacities

Pn, kip

1794.06

Mny, kip-ft

2961.61

Mnx, kip-ft

21139.26

ϕPn, kip

1614.65

ϕMny, kip-ft

2665.45

ϕMnx, kip-ft

19025.34

* The area of the reinforcement in this layer has been included in the area used to compute Cc. As a result, 0.85fc is subtracted from fs in the computation of Fs.