I have a small “T” section that will be a fabricated section. I’m a bit embarrassed, but I can’t seem to remember how to calculate the “J” for a section (always been able to pull the value from the tables). It is needed for Lateral Torsional buckling equations for a tee section in the 13th edition of the AISC. Can anyone out there help me out.
Thanks,
Joe
Assuming J is the Torsion Constant. Then for open sections approximately
J = sum( bt^3/3)
Where b = length of element
T = thickness
For special case of circular section J equals the polar second moment of area.
Regards
Conrad Harrison
B.Tech (mfg & mech), MIIE, gradTIEAust
Adelaide
South Australia
"J" is the polar moment of inertia.
It is the square root of summation of square of moment of inertia
about "x-axis" and "y-axis".
You can find it in any standard Handbook.
Regards,
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> "J" is the polar moment of inertia.
For structural purposes J is the torsional stiffness. The polar
moment of inertia is the torsional stiffness only for the special
case of circular sections
>
> It is the square root of summation of square of moment of inertia
> about "x-axis" and "y-axis".
The polar moment of inertia is the sum of the cross-sectional moments
of inertia, not the root-sum-square
> You can find it in any standard Handbook.
Blodgett is your best resource. It explains everything
Just so you'll know.
Christopher Wright P.E. |"They couldn't hit an elephant at
chr...@skypoint.com | this distance" (last words of Gen.
.......................................| John Sedgwick, Spotsylvania
1864)
http://www.skypoint.com/members/chrisw/