1. Flexibility methods (also known as force methods, compatibility methods or the method of consistent deformations) and

2. Displacement methods (also known as stiffness or equilibrium method)

Each method involves the combination of a

*particular solution*which is obtained by making the structure statically determinate, and a

*complementary solution*in which the effects of each individual modification is assessed. In the force methods, the behaviour of the structure is considered in terms of unknown forces, while in the stiffness method, the behaviour of the structure is considered in terms of unknown displacements. By implication, both analysis methods always involve reducing the structure to a basic system (a determinate system). In the force method, the basic system involves the removal of redundant forces, while the stiffness method involves restraining the joints of the structure against displacement.

In the solved example downloadable from this post, the frame shown above has been analysed for bending moment due to externally applied load using force method and displacement method. In the force method, the graphical method was employed (Vereschagin's rule of diagram multiplication).

To get yourself familiar with Vereschagin's rule, click HERE.

To see an elaborate example of its application, click HERE;

**Highlights of the solved problem****NOTE: Diagrams are not to scale. Read assigned values**

**(a) USING THE FORCE METHOD**

**Step 1**: Calculate the degree of static indeterminacy of the structure

D = (3M + R) - 3N

Where; M = Number of members; R = Number of support reactions; N = Number of nodes

In this case; D = (3x3 + 5) - (3 x 4) = 2

Therefore the structure in indeterminate to the 2nd order

**Step 2**: Reduce the structure to a basic/primary system by removing redundant supports and replacing them with unit loads (X

_{1}and X

_{2})

**Step 3**: Analyse the primary system for the various unit loads, treating each as a separate load case.

*Case 1*

*Case 2***Step 4**: Analyse the primary system when subjected to the external load, and plot the internal forces diagram

**Step 5**: Compute the influence coefficients by diagram multiplication

A few examples of how the bending moment diagrams from above are combined are shown in the figures below.

**Î´**-

_{11}*Deformation at point 1 due to unit load at point 1*. In this case, the bending moment diagram from case 1 is combining with itself;

**Î´**-

_{12}= Î´_{21}*Deformation at point 1 due to unit load at point 2*(this is equal to the deformation at point 2 due to unit load at point 1). In this case, the bending moment from case 1 is combining with diagram from case 2.

**Î´**-

_{22}*Deformation at point 2 due to unit load at point 2*. Here, case 2 bending moment diagram is combining with itself;

**Î”**-

_{1P}*Deformation at point 1 due to externally applied load*. Here, the bending moment from case 1 is combining with bending moment from externally applied load.

**Î”**-

_{2P}*Deformation at point 2 due to externally applied load*. Here, the bending moment from case 2 is combining with bending moment from externally applied load.

**Step 6**: Formulate the appropriate cannonical equation, and solve for the reactive forces X

_{1}and X

_{2}

Î´

_{11}X

_{1}+ Î´

_{12}X

_{2}+ Î”

_{1P}= 0

Î´

_{21}X

_{1}+ Î´

_{22}X

_{2}+ Î”

_{2P}= 0

**Step 7**: Compute the final values of the internal forces

M

_{def}= M

_{0}+ M

_{1}X

_{1}+ M

_{2}X

_{2}

_{ }

**Step 8**: Plot the internal stresses diagram

(

**b) USING THE DISPLACEMENT METHOD**

**Step 1**: Calculate the degree of kinematic indeterminacy. This is the number of unknown nodal displacements that the structure can undergo. They are generally nodal rotations and linear translations. In this example, the structure has unknown displacements at joint C (unknown rotation), joint E (unknown rotation), joint F (unknown rotation), and a lateral displacement (side sway) that is represented at joint F. Therefore it is kinematically indeterminate to the 4th degree.

**Step 2**: Reduce the structure to the primary system by restraining all unknown displacements. Apply unit displacements at the joints so restrained (Z

_{1}, Z

_{2}, Z

_{3}and Z

_{4})

**Step 3**: Analyse the structure for the various unit displacements, treating each as a separate load case.

*Case 1; Z*_{1}= 1.0

*Case 2; Z*_{2}= 1.0

*Case 3; Z*_{3}= 1.0

*Case 4; Z*_{4}= 1.0**Step 4**: Compute the stiffness coefficients for each load case by considering reactions due to unit displacement at the fixed ends. In all cases, K

*ij*stands for the force at point

*i*due to unit displacement at point

*j*.

**Step 5**: Compute the free terms of the cannonical equation for each node from fixed end moments and reactive forces due to externally applied load

**Step 6**: Formulate the appropriate cannonical equation, and solve for the real nodal displacements

Solve for Z

_{1}, Z

_{2}, Z

_{3}, and Z

_{4}

_{ }

**Step 7**: Substitute back and obtain the final values of the bending moment

M

_{def}= M

_{O}+ M

_{1}Z

_{1}+ M

_{2}Z

_{2}+ M

_{3}Z

_{3}+ M

_{4}Z

_{4}

_{ }

**Step 8**: Plot the internal stresses diagram

To download the full solved paper in printable PDF format, click HERE

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