Axially Loaded Member and Tensile Stress oh so lost

AI Thread Summary
To calculate the tensile stress at sections (1) and (2) of an axially loaded member with a load of 1590 N and a thickness of 5 mm, the normal stress equation, normal stress = P/A, is applied. The cross-sectional areas for each section are determined by multiplying the width by the thickness, with section 1 having an area of 0.15 m² and section 2 an area of 0.05 m². The resulting tensile stresses are calculated as 10,600 N/m² for section 1 and 31,800 N/m² for section 2. The discussion emphasizes that this is a straightforward application of the theory of uniaxial tension, with no additional complexities involved. Understanding the basic calculations leads to clarity in solving similar problems.
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Homework Statement


"The axial load for a given test sample carries 1590 N. Calculate tensile stress at sections (1) and (2) assuming the sample thickness is 5mm. (Rectangular cross section).

http://img208.imageshack.us/img208/121/tensilestressby1.th.jpg


Homework Equations


normal stress = P/A
Pallow = (normal stress)allow * A


The Attempt at a Solution


This is a new one for me. All the previous homework problems involved a prismatic bar (a bar of uniform cross-section) and not this 'necked' bar.

Since P are pulling forces, the bar is in tension.

I know my first step would be to convert 5mm into meters = 0.005m

But then I'm sort of lost.

Do I just use the normal stress equation above for each section; 1 and 2? Keeping P = 1590N and then changing A for section 1 to 30mm = 0.03m, and for section 2 to 10mm = 0.01m?

But then where does 5mm come into play?

Thanks for all the help.
 
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You will use the cross sectional area at both locations to calculate the normal stresses. The 5mm is required to calculate the area. The 30 mm and 10 mm dimensions are not areas. How do you calculate the area of a rectangle?
 
Area of a rectangle is length * width

So at section 1, the area A would be 30mm*5mm = 150mm = 0.15m ?
and
Section 2, the area A would be 10mm*5mm = 50mm = 0.05m ?

Then I would just plug those areas into the normal stress = P/A equation for both sections?

Thanks for the quick reply
 
Those above areas should read m^2 and not just meters.
 
normal stress of section 1 = 1590N / 0.15m^2 = 10600 N/m^2
normal stress of section 2 = 1590N / 0.05m^2 = 31800 N/m^2

Could it be that easy? Feel like I'm missing something still
 
It is in this case. You will never see an easier theoretical state of stress than that of a uniaxial tension test. There is no shear until you start dealing with transformations and Mohr's Circle stuff.
 
Wow, well I expected that to be worse.

Thank you very much
 
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