A loaded, simply supported beam is shown below. For this beam:
A. Draw a Free Body Diagram of
the beam, showing all external loads and support forces
(reactions).
B. Determine expressions for the internal shear forces
and bending moments in each sections of the beam.
C. Make shear force and bending moment diagrams for the
beam.
Unless otherwise indicated, all
joints and support points are assumed to be pinned or hinged
joints.

Solution:
Part A:
STEP 1: Draw a free body diagram showing and labeling
all load forces and support (reaction) forces, as well as any
needed angles and dimensions.
STEP 2: Break any forces not already in x and y
direction into their x and y components.
STEP 3: Apply the equilibrium conditions.
Sum Fy = (-1,000 lbs/ft)(4 ft) -
(1,500 lbs/ft)(4 ft) + By + Cy = 0
Sum TB = (Cy)(6 ft) + (1,000
lbs/ft)(4 ft)(2 ft) - (1,500 lbs/ft)(4 ft)(8 ft) = 0
Solving for the unknowns:
Cy
= 6,670 lbs; By =
3,330 lbs
Part B: Determine the Shear Forces and Bending Moments
expressions for each section of the loaded beam. For this process
we will cut the beam into sections, and then use
Statics - Sum of Forces to determine the Shear Force expressions,
and Integration
to determine the Bending Moment expressions in each section of
the beam.
Section 1: Cut the beam at x, where 0 < x < 4 ft. Analyze left hand section.
1. FBD. (Shown in Diagram)
2. All forces in x & y components (yes)
3. Apply translational equilibrium conditions (forces
only):
Sum Fx = 0 (no net external x- forces)
Sum Fy = -1,000 lbs/ft(x) - V1 = 0
Solving: V1 = -1,000x lbs
4. Integration ![]()
M1 = -500 x2 + C1
a)Boundary condition to find
C1: at x=0 M=0
Apply BC: 0 = -500(0)2 + C1
Solving: C1
= 0
Therefore
M1
= [-500x2] ft-lbs for 0 < x < 4 ft.
Section 2: Cut the beam at x, where 4 < x <
10 ft. Analyze left hand section.
1. FBD. (Shown in Diagram)
2. All forces in x & y components (yes)
3. Apply translational equilibrium conditions (forces
only):
Sum Fx = 0 (no net external x- forces)
Sum Fy = -1,000 lbs/ft (4 ft) + 3,330 lbs - V2 = 0
Solving: V2 =
-667 lbs
4. Integration![]()
M2 = -667x + C2
a)Boundary condition to find
C2: at x=4 ft M=-8000 ft-lbs (from equation M1)
Apply BC: 8000 ft-lbs = -667(4) + C2
Solving: C2 = -5,330 ft-lbs
Therefore
M2
= [-667x - 5,330] ft-lbs for 4 < x
< 10
Section 3: Cut the beam at x, where 10 < x
< 14 ft. Analyze left hand section.
1. FBD. (Shown in Diagram)
2. All forces in x & y components (yes)
3. Apply translational equilibrium conditions (forces
only):
Sum Fx = 0 (no net external x- forces)
Sum Fy = -1,000 lbs/ft(4 ft) + 3,330 lbs + 6,670 lbs
-1500lbs/ft(x-10)ft - V3 = 0
Solving: V3 = [-1,500x + 21,000] lbs
4. Integration![]()
M3 = -750x2 + 21,000x + C3
a)Boundary condition to find
C3: at x=14 ft M=0 ft-lbs (end of beam, no external torque so
M3=0)
Apply BC: 0 = -750(14)2 + 21,000(14) + C3
Solving: C3 = -147,000 ft-lbs
Therefore
M3
= [-750x2 + 21,000x - 147,000] ft-lbs for 10 < x < 14
Part C: Shear Force and Bending Moment Diagrams: Now using the expressions found in Part B above, we can draw the shear force and bending moment diagrams for our loaded beam.
V1 = -1,000x lb, V2 = -667 lb, V3 = -1,500x+21,000 lb
M1 = -500x2
ft-lb, M2 = -667x-5,330 ft-lb, M3 = -750x2+21,000x-147,000
ft-lb

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