Factor of safety/principal stress

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The discussion focuses on calculating the revised factor of safety for a shaft subjected to an additional thrust force of 5000N. The initial factor of safety was determined to be 2, with a shear stress of 250MPa and a diameter of 36mm. Participants discuss the correct application of principal stress formulas and the conversion of force to stress, emphasizing the importance of understanding the maximum distortion energy theory for better accuracy. Clarifications are made regarding the calculation of stress and whether other axial stresses are acting on the shaft. The conversation highlights the need for precise calculations and material specifications to ensure accurate safety assessments.
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Homework Statement


After the shaft is manufactured you are informed by the client that the shaft is subjected to an additional thrust force of 5000N. Provide a revised factor of safety for the client.

Found the previous factor of safety to equal 2
Shear stress τ = 250MPa
Diameter = 36mm


Homework Equations



Principal stress formula: σ1,σ2= 0.5(σy+σx) +/- 0.5 x ( sqrt{(σy - σx)^2 + 4τ^2} )


The Attempt at a Solution



σx i assume is 5000N which has to be converted into MPa so I've divided the force by the area ... 5000/ ∏x (18/1000)^2 = 4.9MPa ( i don't know if I've done that conversion correctly for starters)

τxy I'm assuming moves in a clockwise direction so its positive = 250MPa

gonna assume σy = 0 as it doesn't give us any value for that.

Already its starting to look a bit strange, i'd of assumed σx would be larger than τxy but i plugged it into the formula anyway to see what i'd get 252Mpa for σ1

I got to this point and got stuck, the values are most likely wrong but i think the steps are along the right lines, but how do you get a revised factor of safety from this?
 
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Found the previous factor of safety to equal 2
Shear stress tau_xy = 250MPa

I assume some calcs were done to get these values...

Principal stress formula: σ1,σ2= 0.5(σy+σx) +/- 0.5 x ( sqrt{(σy - σx)^2 + 4τ^2} )
This value is an estimate for peak stresses and is a more conservative approach.
From my experience it is better to use the maximum distortion energy theory:
σ_1,σ_2 = ((σ_x-σ_y)⁄2)±sqrt(((σ_x-σ_y)⁄2)^2+τ_xy^2 )
this gives you a better approximation of the Von Mises stresses present.

You don't have to convert the force you simply calculate the stress associated with this force on a specific area. You're calculation is however correct.

σ_x=F/A. This however is just the addisional stress. Is this the only axial stress working in on the shaft?

What material is the shaft made of? I am in quite a hurry, having a meeting in 5 minutes. Will help you further tomorrow, but you have a fairly good idea...
 
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