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Tensile Strength Question



 
 
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  #1  
Old January 10th 06, 07:55 PM posted to rec.aviation.homebuilt
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Default Tensile Strength Question

The 124 KSI strap will have less elongation than the 80 KSI
strap and will therefore take more of the applied load, with the
combination failing much closer to the 124 KSI figure than the
collective 204 KSI limit. When the 124 strap fails, the 80 strap will
stretch and fail almost instantly.
That's how I'd see it, anyway.

Dan

  #3  
Old January 13th 06, 04:02 AM posted to rec.aviation.homebuilt
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Default Tensile Strength Question



Youngs modulus is virtually independent of alloy and heat treat
condition. The load vs elongation will be "the same" if they are the
same size.


I was wondering when someone was going to point this out.

The slope of the stress /strain curve is independent of heat treatment. Both
stretch the same amount with the same force applied. The stronger stuff just
stretches further before it breaks.


  #4  
Old January 16th 06, 05:42 AM posted to rec.aviation.homebuilt
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Default Tensile Strength Question

Thanks ,

That makes much more sense!

Cam.


Youngs modulus is virtually independent of alloy and heat treat
condition. The load vs elongation will be "the same" if they are the
same size.


I was wondering when someone was going to point this out.

The slope of the stress /strain curve is independent of heat treatment. Both stretch the same
amount with the same force applied. The stronger stuff just stretches further before it breaks.



 




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