Mechanics of Materials: find combined loading

In summary, "Mechanics of Materials: find combined loading" focuses on analyzing materials subjected to multiple types of loads simultaneously, such as axial, bending, and torsional loads. It emphasizes the importance of understanding how these loads interact and affect material behavior, leading to stress and strain calculations. The text typically covers key principles, methods for determining resultant stresses, and the application of failure theories to ensure structural integrity under combined loading conditions.
  • #1
SoylentBlue
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Homework Statement
This is not a homework assignment. I am studying civil engineering by myself.
Relevant Equations
Sum of the moments when you cut a beam, as shown above.
TL;DR Summary: A frame with a triangular distributed load is pin-connected to a 2-force member. Find the combined stress at point E on the frame.

problems838-39.jpg
Problem8-39solution.jpg


I am stuck at determining the value of M at the cut. The book shows the value at 8.25KN-meter, but I cannot see how they arrived at that number.
Thank you in advance. I am trying to learn this on my own, so the Internet is my professor right now.
 
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  • #2
Begin by writing the shear ##V## as a function of ##x##. To do this use the definition:

$$ \int dV = -\int w(x)~dx $$

Be careful writing ##w(x)##. The value of the distributed load at distance ##x## from ##A## is that of a line passing through the origin. Write the equation of that line, and integrate on the left from ##V_o## to ##V## ( note initial conditions of ##V## are not zero), and on the right from ##0## to ##x##.

Once you have obtained ##V(x)##, integrate once more to obtain ##M(x)##.
 
  • #3
SoylentBlue said:
Homework Statement: This is not a homework assignment. I am studying civil engineering by myself.
Relevant Equations: Sum of the moments when you cut a beam, as shown above.

TL;DR Summary: A frame with a triangular distributed load is pin-connected to a 2-force member. Find the combined stress at point E on the frame.

View attachment 335991View attachment 335992

I am stuck at determining the value of M at the cut. The book shows the value at 8.25KN-meter, but I cannot see how they arrived at that number.
Thank you in advance. I am trying to learn this on my own, so the Internet is my professor right now.
What you are currently trying to do, you have incorrectly calculated the effective load. What is the value of the distributed load evaluated at ##x = 1.5 ~\rm{m}## ( i.e. ##w( 1.5 ~ \rm{m} ) ~\rm{ \frac{[kN]}{[m]}}##)?
 
  • #4
erobz said:
Begin by writing the shear ##V## as a function of ##x##. To do this use the definition:

$$ \int dV = -\int w(x)~dx $$

Be careful writing ##w(x)##. The value of the distributed load at distance ##x## from ##A## is that of a line passing through the origin. Write the equation of that line, and integrate on the left from ##V_o## to ##V## ( note initial conditions of ##V## are not zero), and on the right from ##0## to ##x##.

Once you have obtained ##V(x)##, integrate once more to obtain ##M(x)##.
OK, so the equation for the load is simply y=4x.
To obtain shear, integrate y=4x to yield y=2x2.
At a value of x=1.5, the shear is 4.5KN, which agrees with the book's answer key.
Is this correct so far?
Integrate again and you get y=2x3/3.
At a value of 1.5, this yields a moment of 2.25 KNmeters.

I'm still a little foggy on how these pieces fit together. In a statics video using a single triangular distributed load, the instructor mentioned several times that the moment curve is the integral of the shear curve. But when he solved for the moment he did not use those relationships. Instead he cut the beam and examined the left side; he used Mcut - (distance to origin)*Ay (where Ay is the upward force at the origin) plus 0.5 (the centroid of the triangle)*concentrated load.
The book's answer key shows a triangular distributed load of 2kN/m at 1.5 meters. I'm not sure how we jumped from 4kN/m to 2kN/m using the shear-moment diagram and the intregrals.
Thank you again...all help is appreciated!! :^)
 

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  • #5
OK, for anyone else who is stuck here, I found the answer in another youtube video:

The equation of our line is y=mx+b. b=0. m is the slope, which they call 4KN/3m when you examine the left-most 3 meters of the load (back to that in a, ahem, moment. Sorry, I just couldn't resist making that pun).
So the equation of our line is y= 4/3x.
V=6 - integral of 4/3xdx = 6- 4/3 x2/2 = 6 - 2/3 x2
For x = 1.5, V = 6 -2/3(1.5)2 = 4.5, which agrees with the book's answer key.
To get the moment, we integrate again: M = integral of 2/3x2dx = 2/3 x3/3 = 2/9x3. For x=1.5, we get a moment of 0.75, which, when subtracted from the moment of 9kNmeters, yields 8.25 kNmeters, which agrees with the book's answer key.

And yes, I realize I drew the moment diagram incorrectly; it should look like an upside-down U.

So, back to that determination of the slope. When I see 4KN/m, I assume 4KN rise per meter of run, or a slope of 4. They show a triangle 3 meters wide and 4 KN tall, and call the slope 4/3. Can anyone comment on this please? Thank you.
 
  • #6
They show a peak distributed load value of 4 kN/m @ x = 3m. It is not 4kN load at x=3m.
 
  • #7
  • #8
erobz said:
They show a peak distributed load value of 4 kN/m @ x = 3m. It is not 4kN load at x=3m.
Oh, thank you!!! That was a subtlety that I had missed. And it obviously had a profound effect on the calculations. Thank you again.
 
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FAQ: Mechanics of Materials: find combined loading

What is combined loading in the context of mechanics of materials?

Combined loading refers to the situation where multiple types of loads (such as axial, torsional, and bending loads) act simultaneously on a structural member. This requires a comprehensive analysis to determine the resultant stresses and deformations.

How do you calculate the normal stress under combined loading?

To calculate the normal stress under combined loading, you need to sum the contributions from each type of load. For axial loads, use σ = P/A, where P is the axial force and A is the cross-sectional area. For bending loads, use σ = My/I, where M is the bending moment, y is the distance from the neutral axis, and I is the moment of inertia. The total normal stress is the sum of these individual stresses.

What is the significance of the superposition principle in combined loading?

The superposition principle is significant in combined loading because it allows for the separate calculation of stresses and deformations due to individual loads, which can then be summed to find the total effect. This principle is valid as long as the material remains within the elastic range and the deformations are small.

How do you determine the shear stress in a member subjected to combined loading?

To determine the shear stress in a member subjected to combined loading, you need to consider the contributions from both transverse shear forces and torsional loads. The shear stress due to a transverse shear force V is τ = VQ/It, where Q is the first moment of the area, I is the moment of inertia, and t is the thickness of the section. The shear stress due to torsion is τ = Tρ/J, where T is the torque, ρ is the radial distance from the center, and J is the polar moment of inertia. The total shear stress is the sum of these individual stresses.

How do you evaluate the combined stress state at a point within a material?

To evaluate the combined stress state at a point within a material, you need to determine both the normal and shear stresses acting on that point. These stresses can then be represented on a stress element and analyzed using Mohr's circle to find the principal stresses and maximum shear stresses. This helps in assessing the material's safety and performance under the given loading conditions.

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