CivilSigma
Structural
- Nov 16, 2016
- 100
Suppose you have a laterally unsupported, simply supported wide flange beam subject to a uniform load. At mid span you also have a torsional moment due to a point load eccentricity.
Design equations in the Canadian code (CSA S16) tell you how to calculate Mr as related to uniform loading only.
How do you verify that the beam can also resist the torsional moment applied?
I know that you can perform a detailed finite element analysis using the Vlasov theory to determine the true Mr of the beam under the above loading conditions.
But is there a simpler "code" approach to the design? Is it reasonable to consider the total factored moment in the beam as: M_f = M_uniform + M_torsion , and then make sure Mr > Mf using the code design equations?
Design equations in the Canadian code (CSA S16) tell you how to calculate Mr as related to uniform loading only.
How do you verify that the beam can also resist the torsional moment applied?
I know that you can perform a detailed finite element analysis using the Vlasov theory to determine the true Mr of the beam under the above loading conditions.
But is there a simpler "code" approach to the design? Is it reasonable to consider the total factored moment in the beam as: M_f = M_uniform + M_torsion , and then make sure Mr > Mf using the code design equations?