Stress Problem Solution for Homework with Simple Equations

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yecko
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Homework Statement


螢幕快照 2018-04-07 下午6.09.28.png


Homework Equations


δ=PL/AE
σ=Eε

The Attempt at a Solution


a: (2L-x)/x
b: For AC, force acting on it = 2P*x/(2L-x) ##linearly proportional
δ=(2P*x/(2L-x))*(2L-x)/[(πD^2/4)*E]=(8P*x)/[(πD^2)*E]

am i wrong in part b?
thanks
 

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yecko said:
a: (2L-x)/x
That makes σ12 when x<L. Does that seem right?
yecko said:
For AC, force acting on it = 2P*x/(2L-x) ##linearly proportional
How do you arrive at that?
Wouldn't it be more useful to write the force required to extend AC by δ in terms of D, E and δ?
 
haruspex said:
Wouldn't it be more useful to write the force required to extend AC by δ in terms of D, E and δ?
as δ is the final answer required, force is just a medium for expressing as part of δ
Chestermiller said:
Kinematically, if the downward displacement of point C is δδ\delta, what is the tensile strain in AC?
ε=δ/(2L-x)
Chestermiller said:
From Hooke's law, what is the tensile stress in AC? In BC?
σ=Eε=Eδ/(2L-x)
haruspex said:
That makes σ1>σ2 when x<L. Does that seem right?
so that should it be x/(2L-x) for part a?

what about part b, what should I do?
thanks
 
yecko said:
as δ is the final answer required, force is just a medium for expressing as part of δ
I don't get your point.
I am suggesting that you can find the force needed to extend the upper part by δ, as a function of δ, D, E etc., and the force required to compress the lower part by δ in the same way. 2P is then the sum of these forces.
You have not explained how you arrived at 2Px/(2L-x).
yecko said:
so that should it be x/(2L-x) for part a?
That sounds like a guess. Can you show some logic to arrive at that?
 
haruspex said:
That sounds like a guess. Can you show some logic to arrive at that?
yecko said:
σ=Eε=Eδ/(2L-x)
From this, the length is inversely proportional to the stress
haruspex said:
I am suggesting that you can find the force needed to extend the upper part by δ, as a function of δ, D, E etc., and the force required to compress the lower part by δ in the same way. 2P is then the sum of these forces.
I am not sure what do you mean by that... let me try

By δ=PL/AE
F1*(2L-x)/AE -F2*x/AE = 0 ---equation 1
F1+ F2 = 2P --- equation 2
F2 = (4PL-2Px)/(1+2L-x)
F1=2P-(4PL-2Px)/(1+2L-x)

therefore δ=(4PL-2Px)/(1+2L-x)*x/[(πD^2/4)E]
is it correct? thanks
 
Chestermiller said:
What is the magnitude and direction of the reaction force at A (in terms of ##\delta##)? At B?
σ=F/A
σ1=R1/A
By σ=Eε=Eδ/L
σ1=Eδ/(2L-x)=R1/A
R1=Eδ/(2L-x)*A
similarly R2=Eδ/x*A
 
Chestermiller said:
In terms of these reaction forces and the force 2P, what is the overall force balance on the rod?
R1+R2+2P=0
Eδ/(2L-x)*A+Eδ/x*A+2P=0
δAE[1/(2L-x)+1/x]+2P=0
δE(πD^2/4)[1/(2L-x)+1/x]+2P=0
δ=-2P/{E(πD^2/4)[1/(2L-x)+1/x]}
is it something like this? thanks
 
yecko said:
R1+R2+2P=0
Eδ/(2L-x)*A+Eδ/x*A+2P=0
δAE[1/(2L-x)+1/x]+2P=0
δE(πD^2/4)[1/(2L-x)+1/x]+2P=0
δ=-2P/{E(πD^2/4)[1/(2L-x)+1/x]}
is it something like this? thanks
Ya see, this is why I asked you for the directions of the reaction forces. Now, again, of ##\delta## is downward, what are the directions of the reaction forces at A and B? So, what is the sign of ##\delta##?
 
Chestermiller said:
Ya see, this is why I asked you for the directions of the reaction forces. Now, again, of ##\delta## is downward, what are the directions of the reaction forces at A and B? So, what is the sign of ##\delta##?
R2 is upward and R1 is downward i guess

R1-R2+2P=0
Eδ/(2L-x)*A-Eδ/x*A+2P=0
δAE[1/(2L-x)-1/x]+2P=0
δE(πD^2/4)[1/(2L-x)-1/x]+2P=0
δ=-2P/{E(πD^2/4)[1/(2L-x)-1/x]}
now, is it something like this? thanks
 
R1+R2-2P=0
Eδ/(2L-x)*A+Eδ/x*A-2P=0
δAE[1/(2L-x)+1/x]-2P=0
δE(πD^2/4)[1/(2L-x)+1/x]=2P
δ=2P/{E(πD^2/4)[1/(2L-x)+1/x]}
now should it be something like this? thanks
 
yecko said:
R1+R2-2P=0
Eδ/(2L-x)*A+Eδ/x*A-2P=0
δAE[1/(2L-x)+1/x]-2P=0
δE(πD^2/4)[1/(2L-x)+1/x]=2P
δ=2P/{E(πD^2/4)[1/(2L-x)+1/x]}
now should it be something like this? thanks
Technically, yes. But, I would have reduced the equation to a simpler mathematical form with a least common denominator:
$$\delta=\frac{4Px(2L-x)}{\pi D^2LE}$$