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? + = EI EI M
C DC
3
2
3
2
?    (3) 
 
Now, consider the joint equilibrium of B andC (vide Fig. 17.3c). 
 
0 0 = + ? =
?
BC
BA B
M M M  (4) 
 
      (5) 0 0 = + ? =
?
CD
CB C
M M M
 
 
 
The required third equation is written considering the horizontal equilibrium of the 
entire frame   (vide Fig. 17.3d). . .e i
?
= 0
X
F
 
 
    0 10
2 1
= - + - H H 
       
    10
2 1
= + ? H H .   (6) 
 
 
 
 
Page 2


? + = EI EI M
C DC
3
2
3
2
?    (3) 
 
Now, consider the joint equilibrium of B andC (vide Fig. 17.3c). 
 
0 0 = + ? =
?
BC
BA B
M M M  (4) 
 
      (5) 0 0 = + ? =
?
CD
CB C
M M M
 
 
 
The required third equation is written considering the horizontal equilibrium of the 
entire frame   (vide Fig. 17.3d). . .e i
?
= 0
X
F
 
 
    0 10
2 1
= - + - H H 
       
    10
2 1
= + ? H H .   (6) 
 
 
 
 
 
 
Considering the equilibrium of the column AB andCD , yields 
 
3
1
AB BA
M M
H
+
=      
   
and  
 
     
3
2
DC CD
M M
H
+
=      (7) 
 
The equation (6) may be written as, 
 
30 = + + +
DC CD AB BA
M M M M     (8) 
 
Substituting the beam end moments from equation (3) in equations (4), (5) and 
(6) 
 
10 667 . 0 5 . 0 333 . 2 - = ? + + EI EI EI
C B
? ?  (9) 
 
10 667 . 0 5 . 0 333 . 2 = ? + + EI EI EI
B C
? ?  (10) 
  
 
Page 3


? + = EI EI M
C DC
3
2
3
2
?    (3) 
 
Now, consider the joint equilibrium of B andC (vide Fig. 17.3c). 
 
0 0 = + ? =
?
BC
BA B
M M M  (4) 
 
      (5) 0 0 = + ? =
?
CD
CB C
M M M
 
 
 
The required third equation is written considering the horizontal equilibrium of the 
entire frame   (vide Fig. 17.3d). . .e i
?
= 0
X
F
 
 
    0 10
2 1
= - + - H H 
       
    10
2 1
= + ? H H .   (6) 
 
 
 
 
 
 
Considering the equilibrium of the column AB andCD , yields 
 
3
1
AB BA
M M
H
+
=      
   
and  
 
     
3
2
DC CD
M M
H
+
=      (7) 
 
The equation (6) may be written as, 
 
30 = + + +
DC CD AB BA
M M M M     (8) 
 
Substituting the beam end moments from equation (3) in equations (4), (5) and 
(6) 
 
10 667 . 0 5 . 0 333 . 2 - = ? + + EI EI EI
C B
? ?  (9) 
 
10 667 . 0 5 . 0 333 . 2 = ? + + EI EI EI
B C
? ?  (10) 
  
 
30
3
8
2 2 = ? + + EI EI EI
C B
? ?    (11) 
 
Equations (9), (10) and (11) indicate symmetry and this fact may be noted. This 
may be used as the check in deriving these equations. 
 
Solving equations (9), (10) and (11), 
 
355 . 1 ; 572 . 9 = - =
C B
EI EI ? ?     and    417 . 17 = ? EI . 
 
Substituting the values of 
C B
EI EI ? ? , and ? EI in the slope-deflection equation 
(3), one could calculate beam end moments. Thus, 
 
5.23 kN.m (counterclockwise)
AB
M = 
 
1.14 kN.m(clockwise)
BA
M =- 
 
1.130 kN.m
BC
M = 
 
13.415 kN.m
CB
M =- 
 
13.406 kN.m
CD
M = 
 
12.500 kN.m
DC
M = . 
 
The bending moment diagram for the frame is shown in Fig. 17.3 e. And the 
elastic curve is shown in Fig 17.3 f. the bending moment diagram is drawn on the 
compression side. Also note that the vertical hatching is used to represent 
bending moment diagram for the horizontal members (beams). 
 
 
Page 4


? + = EI EI M
C DC
3
2
3
2
?    (3) 
 
Now, consider the joint equilibrium of B andC (vide Fig. 17.3c). 
 
0 0 = + ? =
?
BC
BA B
M M M  (4) 
 
      (5) 0 0 = + ? =
?
CD
CB C
M M M
 
 
 
The required third equation is written considering the horizontal equilibrium of the 
entire frame   (vide Fig. 17.3d). . .e i
?
= 0
X
F
 
 
    0 10
2 1
= - + - H H 
       
    10
2 1
= + ? H H .   (6) 
 
 
 
 
 
 
Considering the equilibrium of the column AB andCD , yields 
 
3
1
AB BA
M M
H
+
=      
   
and  
 
     
3
2
DC CD
M M
H
+
=      (7) 
 
The equation (6) may be written as, 
 
30 = + + +
DC CD AB BA
M M M M     (8) 
 
Substituting the beam end moments from equation (3) in equations (4), (5) and 
(6) 
 
10 667 . 0 5 . 0 333 . 2 - = ? + + EI EI EI
C B
? ?  (9) 
 
10 667 . 0 5 . 0 333 . 2 = ? + + EI EI EI
B C
? ?  (10) 
  
 
30
3
8
2 2 = ? + + EI EI EI
C B
? ?    (11) 
 
Equations (9), (10) and (11) indicate symmetry and this fact may be noted. This 
may be used as the check in deriving these equations. 
 
Solving equations (9), (10) and (11), 
 
355 . 1 ; 572 . 9 = - =
C B
EI EI ? ?     and    417 . 17 = ? EI . 
 
Substituting the values of 
C B
EI EI ? ? , and ? EI in the slope-deflection equation 
(3), one could calculate beam end moments. Thus, 
 
5.23 kN.m (counterclockwise)
AB
M = 
 
1.14 kN.m(clockwise)
BA
M =- 
 
1.130 kN.m
BC
M = 
 
13.415 kN.m
CB
M =- 
 
13.406 kN.m
CD
M = 
 
12.500 kN.m
DC
M = . 
 
The bending moment diagram for the frame is shown in Fig. 17.3 e. And the 
elastic curve is shown in Fig 17.3 f. the bending moment diagram is drawn on the 
compression side. Also note that the vertical hatching is used to represent 
bending moment diagram for the horizontal members (beams). 
 
 
 
 
Page 5


? + = EI EI M
C DC
3
2
3
2
?    (3) 
 
Now, consider the joint equilibrium of B andC (vide Fig. 17.3c). 
 
0 0 = + ? =
?
BC
BA B
M M M  (4) 
 
      (5) 0 0 = + ? =
?
CD
CB C
M M M
 
 
 
The required third equation is written considering the horizontal equilibrium of the 
entire frame   (vide Fig. 17.3d). . .e i
?
= 0
X
F
 
 
    0 10
2 1
= - + - H H 
       
    10
2 1
= + ? H H .   (6) 
 
 
 
 
 
 
Considering the equilibrium of the column AB andCD , yields 
 
3
1
AB BA
M M
H
+
=      
   
and  
 
     
3
2
DC CD
M M
H
+
=      (7) 
 
The equation (6) may be written as, 
 
30 = + + +
DC CD AB BA
M M M M     (8) 
 
Substituting the beam end moments from equation (3) in equations (4), (5) and 
(6) 
 
10 667 . 0 5 . 0 333 . 2 - = ? + + EI EI EI
C B
? ?  (9) 
 
10 667 . 0 5 . 0 333 . 2 = ? + + EI EI EI
B C
? ?  (10) 
  
 
30
3
8
2 2 = ? + + EI EI EI
C B
? ?    (11) 
 
Equations (9), (10) and (11) indicate symmetry and this fact may be noted. This 
may be used as the check in deriving these equations. 
 
Solving equations (9), (10) and (11), 
 
355 . 1 ; 572 . 9 = - =
C B
EI EI ? ?     and    417 . 17 = ? EI . 
 
Substituting the values of 
C B
EI EI ? ? , and ? EI in the slope-deflection equation 
(3), one could calculate beam end moments. Thus, 
 
5.23 kN.m (counterclockwise)
AB
M = 
 
1.14 kN.m(clockwise)
BA
M =- 
 
1.130 kN.m
BC
M = 
 
13.415 kN.m
CB
M =- 
 
13.406 kN.m
CD
M = 
 
12.500 kN.m
DC
M = . 
 
The bending moment diagram for the frame is shown in Fig. 17.3 e. And the 
elastic curve is shown in Fig 17.3 f. the bending moment diagram is drawn on the 
compression side. Also note that the vertical hatching is used to represent 
bending moment diagram for the horizontal members (beams). 
 
 
 
 
 
Example 17.2 
Analyse the rigid frame as shown in Fig. 17.4a and draw the bending moment 
diagram. The moment of inertia for all the members is shown in the figure. 
Neglect axial deformations. 
 
 
 
 
 
 
 
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FAQs on The Slope Deflection Method: Frames with Sidesway - 2 - Structural Analysis - Civil Engineering (CE)

1. What is the slope deflection method in structural analysis?
Ans. The slope deflection method is a technique used in structural analysis to determine the displacements and moments in a structure subjected to loads. It involves calculating the slopes and rotations at the ends of each member, as well as the moments at the ends of each member, by considering the compatibility of deformations and equilibrium of forces.
2. How does the slope deflection method handle frames with sidesway?
Ans. The slope deflection method can handle frames with sidesway by incorporating the concept of sidesway into the analysis. Sidesway refers to the lateral deflection of a frame due to the absence of sufficient stiffness in its lateral direction. In the slope deflection method, additional equations are derived to account for sidesway, considering the bending moments and rotations at each joint due to sidesway effects.
3. What are the advantages of using the slope deflection method for analyzing frames with sidesway?
Ans. The slope deflection method offers several advantages for analyzing frames with sidesway: - It provides a more accurate representation of the behavior of the frame under lateral loads compared to other simplified methods. - It allows for the consideration of frame imperfections, such as initial member deformations and joint rotations, which can significantly affect the structure's response to lateral loads. - It can handle complex frame geometries and loading conditions, making it versatile for various structural analysis scenarios. - It provides detailed information about the internal forces and displacements at each joint, enabling engineers to assess the structural integrity and design more efficient solutions.
4. Are there any limitations or assumptions associated with the slope deflection method for frames with sidesway?
Ans. Yes, there are certain limitations and assumptions associated with the slope deflection method for frames with sidesway: - It assumes that the frame members behave elastically, meaning they do not undergo plastic deformation. - It assumes that the structure is statically determinate, with the number of unknowns equal to the number of equations available for analysis. - It assumes that the sidesway effects can be adequately modeled using additional equations derived from the compatibility of deformations and equilibrium of forces. - It may not accurately capture the behavior of frames with significant non-linearities or large displacements. - It assumes that the frame joints are rigid, neglecting any rotational flexibility or deformations at the joints.
5. How can I apply the slope deflection method to analyze a frame with sidesway?
Ans. To apply the slope deflection method for analyzing a frame with sidesway, follow these steps: 1. Identify the frame members, their lengths, and cross-sectional properties. 2. Determine the support conditions and external loads acting on the frame. 3. Establish the coordinate system and assign positive rotations and displacements. 4. Calculate the fixed-end moments for each member based on the applied loads and support conditions. 5. Set up equilibrium equations for each joint, considering the bending moments, rotations, and sidesway effects. 6. Solve the resulting system of equations to obtain the unknown member rotations and moments. 7. Use the calculated member rotations and moments to determine the joint displacements and internal forces throughout the frame. 8. Verify the results by ensuring compatibility of deformations and equilibrium of forces at each joint. 9. Make any necessary adjustments or iterations to improve the accuracy of the analysis.
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