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Aeronautical Engineering/tensile bar stress distribution

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Question
Hello Ray,

I have two tensile bars with the same cross sectional area.  

One of the tensile bar cross sections happens to be round and the other is rectangular.

Would there be an even distribution in tensile stress for both bars?  Would the corners of the rectangular bar adversely affect the yield and tensile values as compared to the round bar?  Do the corners act like stress risers resulting in a lower UTS and Yield?

Thanks,
Allen

Answer
Hi Allen

The usual assumption is that tensile stresses are evenly distributed across cross sections (provided the difference in cross section isn't extreme), unlike compressive stresses. This should mean that different bars of equal area are equally stressed. This is achieved by a small variation of elastic or plastic deformation to even out the stress across the section. However, I'm not a structural engineer, so don't bet the farm on this one!

Aeronautical Engineering

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Ray Wilkinson

Expertise

aircraft structures; artificial and induced environments - vibration, temperature, altitude, etc; conceptual design of aircraft; systems - hydraulics, electrical; safety, reliability and maintainability; rocketry, particularly propulsion; University admissions (UK only - not able to answer for other countries)

Experience

I teach all of the above at the University of Hertfordshire, UK, as a Principal Lecturer (17 years), previously Senior Engineer at BAe Dynamics (now MBDA) (11 years)

Publications
My own book - Aircraft Structures and Systems, MechAero Publishing
Currently writing a book on rocketry

Education/Credentials
Bachelor of Technology degree in Aeronautical Engineering (1980), Loughborough University, UK

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