Sam P.

asked • 03/05/22

Shear and Moment

Solve for the Shear forces and Moment of each point and Draw its shear and moment diagram.

A simply supported beam with a fixed support(A) at left end and roller support(F) at right end. Point A has no force, Point B has 10 kN, C to D has uniformly distributed load of 20 kN/m, E with 15 kN and F with no force applied.

Distance from point-point:

A-B(1m), B-C(1m), C-D (3m), D-E (2m), and E-F (1m).

Zachary R.

Hi! Could you clarify if all these externally applied forces are acting vertically and, if so, is each one pointing upwards (+y direction) or downwards (-y direction)?
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03/05/22

Sam P.

All externally applied force are acting vertically. They are pointing downwards. Thank you, I hope you can help me.
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03/06/22

1 Expert Answer

By:

Zachary R. answered • 03/06/22

Tutor
4.9 (45)

B.S. in Mechanical Engineering / M.S. in Materials Science & Eng.

Sam P.

Thank you so much for your help🥰 btw, A is a pin-point constraint(my mistake✌).Thanks for giving your time to explain it to me.
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03/06/22

Zachary R.

Ah I see! So a Pin Constraint has one less reaction than a Fixed Constraint (Pins' do not have a reaction moment). So the problem is no longer statically indeterminant.
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03/06/22

Zachary R.

Based on that, here is how you could go about solving for the shear/moment diagrams in one particular beam segment (CD, the one with the uniformly distributed load). Step #1: Use Statics Eq.s on the entire beam to solve for reaction forces Ay and Fy. Sum of Moments about point A = 0 eq.: >> 0 = -(10 kN)(1 m) - (20 kN/m)(3 m)(3.5 m) - (15 kN)(7 m) + (Fy)(8 m) >> Fy = 45 kN *** Sum of Vertical Forces = 0 Eq.: >> 0 = Ay + Fy - (10 kN) - (20 kN/m)(3 m) - (15 kN) >> Ay = 85 - Fy >> Ay = 85 - (45) >> Ay = 40 kN *** Its completely trivial in this problem, but you could use the summation of horizontal forces = 0 equation to prove that the horizontal reaction at A is also zero.
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03/06/22

Zachary R.

Step #2: Imagine that we make a vertical "cut" thru the beam a distance "x" from Point A. For this particular analysis, let's say that this location "x" lies somewhere in the CD segment where the distributed force lies. Let's redraw the free-body diagram, but only the portion of the beam that is to the *left* of our cut at "x". What forces and moments show up on this free-body diagram? From left-to-right we would have (1) Upward Force of Ay = 40 kN at A, (2) downward force of 10 kN at point B, (3) downward distributed force applied from Point C until Point X, (4) a downward *internal* shear force at Point X that we can call V(x), and (5) a counter-clockwise *internal* moment at Point X that we can call M(x).
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03/06/22

Zachary R.

How can we "handle" that weird distributed force from Point C to Point X? Well when we want to do our standard statics equations when there are distributed loads we often times imagine replacing distributed loads with a point load with magnitude equal to the total magnitude of the distributed load, and which is located at the centroid of the distribution. In this case, since the distributed load is uniform, and spans from Point C (2 m along the bar) to Point X ("x" m along the bar) in our new FBD, the equivalent force magnitude would be: (20 kN/m)( x - 2 ). The location of this equivalent force will be in the middle of that distribution, which we can evaluate to be at (2 + (x-2)/2) meters to the right of Point A.
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03/06/22

Zachary R.

Now let's apply our standard statics equations to our smaller FBD, now that we know how to handle that distributed load. Sum of Vertical Forces Equation: >> 0 = (+40 kN) - (10 kN) - (20 kN/m)(x - 2) - V(x) >> V(x) = 30 - 20x + 40 >> V(x) = 70 - 20x *** So the internal shear in this segment of the beam is a linearly decreasing function of position "x" along the beam.
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03/06/22

Zachary R.

To find internal moment ( M(x) ), we just need to apply our Moment statics equation. The trickiest thing here is that the internal shear, V(x), may show up in our equation for M(x), but we can plug in our earlier function for V(x) at the end! Lets do moments about Point A... 0 = -(10 kN)(1 m) - (20 kN/m)( x - 2 )(2 + (x-2)/2) - x*[V(x)] + M(x) ***** M(x) = x*V(x) + 10 + (20)(x - 2)(2 + (x-2)/2) ******* Now plug in our earlier known function for in the internal shear (V(x))... M(x) = x*(70 - 20x) + 10 + (20)(x - 2)(2 + (x-2)/2) ****** This is a correct equation for the internal moment as a function of position x within segment BC. You should definitely simplify this more by distributing all the terms and combining, but it will be a quadratic equation for M(x). If you repeat this process again and again, but for a different cut in each segment of the beam, then youll have the ability to fully draw out a shear and moment diagram for the entire beam.
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03/06/22

Zachary R.

If you have any other questions, or would be interested in statics tutoring, let me know and I'd be happy to help!
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03/06/22

Sam P.

Thank you so much. You're such a big help!
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03/07/22

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