Reduction of a simple distributed loading (correct1)

In summary: M= 4*b*1/2*1/3b+2.5*(b+a)*1/2*1/3*(b+a)filling in 0.6b=a gives M= -2/3b^2+ 5/12(b+0.6b)^2which gives M= 0.4b^2Which can never get below zero. You can graph it or use the D<0...> theorem.
  • #1
Pascal1p
28
0

Homework Statement


View_image_1456412389869.jpg

I am not yet at the chapter of equations of equilibrium, plus it says the couple moment is not 0, so I assume it just about the loadings and not including the reactive forces and reactive moment.

Homework Equations


F= 1/2*b*h
M= 1/2*b*h*d

The Attempt at a Solution


So if I call the top one F1 and the bottom loading F2 I got:

F1+F2=0= -4*b*1/2+2.5*(b+a)*1/2
solving this i got a=0.6b

Moment around the of the bar (not A, but opposite side) due to the loadings is (counter clockwise positive):

M= -F1*center of triangle + F2*center of triangle
Because you can replace the loading with force F1 and force F2 and its line of action is through the center of the triangle area (1/3* base)
M= -8= -4*b*1/2*1/3b+2.5*(b+a)*1/2*1/3*(b+a)

So what am I doing wrong?
Because M can never be negative with me, plus the answer should be b= 5.625 and a= 1.539.
But this to me makes no sense, because then F1+F2 is not 0.
And if I should take the reactive forces into account at A then you can never have still a moment, because then it is not static anymore.
 
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  • #2
Pascal1p said:

Homework Statement


View_image_1456412389869.jpg

I am not yet at the chapter of equations of equilibrium, plus it says the couple moment is not 0, so I assume it just about the loadings and not including the reactive forces and reactive moment.

Homework Equations


F= 1/2*b*h
M= 1/2*b*h*d

The Attempt at a Solution


So if I call the top one F1 and the bottom loading F2 I got:

F1+F2=0= -4*b*1/2+2.5*(b+a)*1/2
solving this i got a=0.6b

I agree with this.
Moment around the of the bar (not A, but opposite side) due to the loadings is (counter clockwise positive):

M= -F1*center of triangle + F2*center of triangle
Because you can replace the loading with force F1 and force F2 and its line of action is through the center of the triangle area (1/3* base)
M= -8= -4*b*1/2*1/3b+2.5*(b+a)*1/2*1/3*(b+a)

So what am I doing wrong?

If your moment convention is negative for CW moments, then you should carry this convention thru your moment calculations.
Because M can never be negative with me, plus the answer should be b= 5.625 and a= 1.539.
But this to me makes no sense, because then F1+F2 is not 0.
And if I should take the reactive forces into account at A then you can never have still a moment, because then it is not static anymore.
The values a = 1.539 and b = 5.625 do not produce a zero net force on the beam with the indicated loadings, so they cannot be correct.

You never said what you calculated for a and b.
 
  • #3
SteamKing said:
I agree with this.If your moment convention is negative for CW moments, then you should carry this convention thru your moment calculations.

The values a = 1.539 and b = 5.625 do not produce a zero net force on the beam with the indicated loadings, so they cannot be correct.

You never said what you calculated for a and b.
But I did carry it though my moment equations?
M=-8 = - F1*d1 + F2* d2
This is what I did, F1 produces a clockwise moment (thus negative sign) and F2 produces a counterclockwise moment (thus positive).

I did not get a value for a and b, since - F1*d1 + F2* d2 never get below 0 if I use M= -8= -4*b*1/2*1/3b+2.5*(b+a)*1/2*1/3*(b+a)
 
  • #4
Pascal1p said:
But I did carry it though my moment equations?
M=-8 = - F1*d1 + F2* d2
This is what I did, F1 produces a clockwise moment (thus negative sign) and F2 produces a counterclockwise moment (thus positive).

I did not get a value for a and b, since - F1*d1 + F2* d2 never get below 0 if I use M= -8= -4*b*1/2*1/3b+2.5*(b+a)*1/2*1/3*(b+a)
I don't know how you can say - F1*d1 + F2* d2 never got below zero because you never showed this to be true and you never worked out a value for a or b.
It really doesn't matter, since the values of a and b which are the supposed "solutions" are incorrect.
 
  • #5
SteamKing said:
I don't know how you can say - F1*d1 + F2* d2 never got below zero because you never showed this to be true and you never worked out a value for a or b.
It really doesn't matter, since the values of a and b which are the supposed "solutions" are incorrect.

well i said a=0.6b, you also found that correct now
M= 4*b*1/2*1/3b+2.5*(b+a)*1/2*1/3*(b+a)
filling in 0.6b=a gives M= -2/3b^2+ 5/12(b+0.6b)^2
which gives M= 0.4b^2
Which can never get below zero. You can graph it or use the D<0 method
 
  • #6
Pascal1p said:
well i said a=0.6b, you also found that correct now
M= 4*b*1/2*1/3b+2.5*(b+a)*1/2*1/3*(b+a)
filling in 0.6b=a gives M= -2/3b^2+ 5/12(b+0.6b)^2
which gives M= 0.4b^2
Which can never get below zero. You can graph it or use the D<0 method
I took moments about the fixed end of the beam. In that case, the top moment was CCW and the bottom moment was CW. I got a net CW moment, which allowed me to solve for a and b, but these were different values than the ones which were supposed to be the solutions.
 
  • #7
Since the downwards forces have an effective line of action to the left of that of the upward forces, the net moment is clearly anticlockwise. You are right, the book is wrong.
 
  • #8
SteamKing said:
I took moments about the fixed end of the beam.
the OP method is simpler.
 

What is the purpose of reducing a simple distributed loading?

The purpose of reducing a simple distributed loading is to simplify the calculation of the total load on a structure or system. This can make it easier to analyze the structural integrity and determine the appropriate measures for reinforcement or support.

What is a simple distributed loading?

A simple distributed loading is a type of load that is spread out evenly over a certain area or length. This is different from a concentrated load, which is applied at a specific point. Simple distributed loading can include things like the weight of a roof or the pressure from wind on a building.

How is a simple distributed loading reduced?

A simple distributed loading can be reduced by converting it into an equivalent concentrated load. This involves calculating the total weight or force of the distributed load and then finding the equivalent point where it can be applied. This point is usually referred to as the centroid or center of gravity.

What are the benefits of reducing a simple distributed loading?

Reducing a simple distributed loading can make it easier to analyze and design structures. It can also help to minimize the effects of the load on the structure, such as stress and deflection. Additionally, reducing a distributed loading can simplify the calculation process and save time.

Are there any limitations to reducing a simple distributed loading?

Yes, there are limitations to reducing a simple distributed loading. This method is only applicable for loads that are evenly distributed. If the load is not evenly distributed, the reduction process may not accurately reflect the actual load on the structure. In these cases, more advanced analysis methods may be necessary.

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