Problem 9.1. Moments of multispan beam

A multispan beam given in the Figure below is subjected at every other span by a uniformly distributed load, p = 4 kN/m. Number of spans is n = 5, length of spans is l = 3 m, bending stiffness, EI of the beam is uniform. Determine the bending moment diagram of the beam with the aid of the force method.

Solve Problem

Solve

Maximum negative moment, Mmax [kNm]=

Positive moment at the middle of the beam, M+ [kNm]=

Do you need help?

Steps
Step by step

Force method is described in Section 9.1.
Step 1.  Define a primary structure. Choose the redundants.

Check figure

The degree of indeterminancy is four. Four hinges are introduced above the intermediate supports, thus the primary structure is a set of simply supported girders. The four redundants are the moment couples, X1, X2, X3, X4 shown in the Figure.

Step 2.  Draw moment diagrams of the primary structure from the original load and from the unit redundants.

Check diagrams

Step 3.  Determine redundants from the compatibility condition.

Check redundants

Compatibility conditions are referred to the relative rotations above the intermediate supports, which must be zero. To calculate the rotations Castigliano’s theorem can be applied.

See Problem 6.6.

Rotations at the supports from the uniformly distributed load is

ai0=0lM0MiEIdx=pL324EI

Derived in Problem 6.6 b)
Relative rotations above the hinges from the unit redudants are

aii=0lMiMiEIdx=2Ai23=2×1×l223=2L3EIai,i+1=0lMiMi+1EIdx=Ai13=1×l213=L6EIai1,i=0lMi1MiEIdx=Ai13=1×l213=L6EI

where ai,i+1 is the relative rotation above the i+1-th support from the i-th unit redundant.

According to the recipocal theorem, we may write:

ai1,i=ai,i1

Compatibilty conditions written for all the four intermediate supports result in a linear equation system, from which the redundants can be calculated:

a10+a11X1+a21X2=0a20+a12X1+a22X2+a23X3=0a30+a23X2+a33X3+a34X4=0a20+a34X3+a44X4=0     a10a20a30a40+a11a2100a12a22a3200a23a33a43a34a44X1X2X3X4 pl324EI 1111+l6EI4100141001410014X1X2X3X4=0      X1X2X3X4=pl24410014100141001411111=pl25.263.953.955.26102=4.0×3.025.263.953.955.26102=1.891.421.421.89kNm

Step 4.  Apply superposition to give the moment diagram of the statically indeterminate structure.

Check result

M=M0+M1X1+M2X2+M3X3+M4X4

The maximum negative moment is

Mmax=X1=1.89 kNm

Positive moment at the middle of the girder is

 

Compare the results to the moments with infinite number of spans. Increasing the number of spans, n  all the redundant would result in

X=Xi=pl224

and the moment diagram would be 

Results
Worked out solution

Force method is described in Section 9.1.
The degree of indeterminancy is four. Four hinges are introduced above the intermediate supports, thus the primary structure is a set of simply supported girders. The four redundants are the moment couples, X1, X2, X3, X4 shown in the Figure.

Moment diagrams of the primary structure from the original load and from the unit redundants are given below.

Redundants are determined from the compatibility condition.The relative rotations above the intermediate supports must be zero. To calculate the rotations Castigliano’s theorem can be applied.

See Problem 6.6.

Rotations at the supports from the uniformly distributed load is

ai0=0lM0MiEIdx=pL324EI

Derived in Problem 6.6 b)
Relative rotations above the hinges from the unit redudants are

aii=0lMiMiEIdx=2Ai23=2×1×l223=2L3EIai,i+1=0lMiMi+1EIdx=Ai13=1×l213=L6EIai1,i=0lMi1MiEIdx=Ai13=1×l213=L6EI

where ai,i+1 is the relative rotation above the i+1-th support from the i-th unit redundant.

According to the recipocal theorem, we may write:

ai1,i=ai,i1

Compatibilty conditions written for all the four intermediate supports result in a linear equation system, from which the redundants can be calculated:

a10+a11X1+a21X2=0a20+a12X1+a22X2+a23X3=0a30+a23X2+a33X3+a34X4=0a20+a34X3+a44X4=0     a10a20a30a40+a11a2100a12a22a3200a23a33a43a34a44X1X2X3X4 pl324EI 1111+l6EI4100141001410014X1X2X3X4=0      X1X2X3X4=pl24410014100141001411111=pl25.263.953.955.26102=4.0×3.025.263.953.955.26102=1.891.421.421.89kNm

Moment diagram of the statically indeterminate structure is obtained by superposition.

M=M0+M1X1+M2X2+M3X3+M4X4

The maximum negative moment is

Mmax=X1=1.89 kNm

Positive moment at the middle of the girder is

M+=M0+M2X2+M3X3=pl2812X212X2=4.0×3.02821.422=3.08 kNm

The results are compared to the moments with infinite number of spans. Increasing the number of spans, n  all the redundant would result in

X=Xi=pl224

and the moment diagram would be