RAM Connection Column Splice - Demand Calculation

Hello,

How does RAM Connection determine the demand values of 39.16 kip-ft (highlighted in red on the 2nd image below)? This is a column splice for two W40x264 columns (top and bottom) subjected to a weak axis moment (M2) of 40 kip-ft.

Thank you

Parents
  • Have you tried using the "View Formulas" button at the top of the results? Often that'll show more calculations and code references than the standard view.
  • Yes, but that doesn't show the demand calculations. That only shows the formulas used for the capacity calculations.
  • Gotcha - I wasn't sure about that particular connection type - some types do show demand calcs.

    Good Luck.
  • The development is reviewing this. We will post more information soon.



  • RAM Connection follows the recommendations from “Handbook of Structural Steel Connection Design and Details” by Akbar R. Tamboli” for AISC column splices. Specifically Section 2.2.5 Splices – columns and truss chords, from page 115 to 123.

    The simplest method for designing column splices for biaxial bending is to establish a flange force (required strength) which is statically equivalent to the applied moments and then to design the bolts, welds, plates, and fillers (if required) for this force. For minor axis bending, the force F needs to be distributed over some finite bearing area as shown in figure:

    The bearing area is (2∙ε∙t) where t is the thickness of the inner flange, ε is the position of the force, F, from the toe of the flange of the smaller column, and T is the forcer per gage line of bolts. The quantities T and F are for each of the two flanges. If My is the weak axis applied moment, Mf = My/2 is the weak axis applied moment per flange.

    The bearing area is determined by requiring that the bearing stress reaches its design strength at the load, F. Thus, 0.75 (1.8Fy)(2 ε)t = F, and since from vertical equilibrium F = 2T and 0.75 (1.8 Fy) t ε = T.

    Thus, Mf = 0.75 (1.8 Fy) t ε (b – 2 ε)

    And solving for ε:

    Where Mpy = Fy Zy = ½ Fy t b^2. This expression for ε is valid as long as:

    When Mf > 3/8 φ Mpy, the tension, T, on the bolts on the bearing side vanishes and the next figure applies. In this case, F = T = 0.75 (1.8 Fy) t (2 ε).

    And

     

    Where γ = 1 + g/b. This expression for ε is valid as long as:

    But T need can never exceed Mf/g. The flange force in every case is Ffy = 2T. Using the user’s model data:

    g = 0.5 in.

    Mf = 40 kips / 2 = 20 kips.

    Mpy = Zy * Fy = 0.07638 * 7200 = 550 Kip*in

    γ = 1 + g/b = 1 + 0.5/0.9916 = 1.5042

    F = 2 T;

    F = 2 * (φ (1.8 Fy) t ε) =  2 * (0.75 * 1.8 * 7200 * 0.1441 * 0.01373 = 38.497 Kips

     

    F max = 2 * Mf / g = 2 * (20 / 0.5) = 80 Kips

    As the flange force does not exceed the maximum, RCnx uses the calculated F value of 38.5 Kips. RAM Connection calculates the maximum flange force acting on the column about either the major or minor axis plus the tension in the in the flange. The user’s model only has data for minor axis calculations. As he noticed, the demand differs when he uses ASD or LFRD and the reason is the calculation has φ as a parameter.

    I hope this helps.



Reply
  • RAM Connection follows the recommendations from “Handbook of Structural Steel Connection Design and Details” by Akbar R. Tamboli” for AISC column splices. Specifically Section 2.2.5 Splices – columns and truss chords, from page 115 to 123.

    The simplest method for designing column splices for biaxial bending is to establish a flange force (required strength) which is statically equivalent to the applied moments and then to design the bolts, welds, plates, and fillers (if required) for this force. For minor axis bending, the force F needs to be distributed over some finite bearing area as shown in figure:

    The bearing area is (2∙ε∙t) where t is the thickness of the inner flange, ε is the position of the force, F, from the toe of the flange of the smaller column, and T is the forcer per gage line of bolts. The quantities T and F are for each of the two flanges. If My is the weak axis applied moment, Mf = My/2 is the weak axis applied moment per flange.

    The bearing area is determined by requiring that the bearing stress reaches its design strength at the load, F. Thus, 0.75 (1.8Fy)(2 ε)t = F, and since from vertical equilibrium F = 2T and 0.75 (1.8 Fy) t ε = T.

    Thus, Mf = 0.75 (1.8 Fy) t ε (b – 2 ε)

    And solving for ε:

    Where Mpy = Fy Zy = ½ Fy t b^2. This expression for ε is valid as long as:

    When Mf > 3/8 φ Mpy, the tension, T, on the bolts on the bearing side vanishes and the next figure applies. In this case, F = T = 0.75 (1.8 Fy) t (2 ε).

    And

     

    Where γ = 1 + g/b. This expression for ε is valid as long as:

    But T need can never exceed Mf/g. The flange force in every case is Ffy = 2T. Using the user’s model data:

    g = 0.5 in.

    Mf = 40 kips / 2 = 20 kips.

    Mpy = Zy * Fy = 0.07638 * 7200 = 550 Kip*in

    γ = 1 + g/b = 1 + 0.5/0.9916 = 1.5042

    F = 2 T;

    F = 2 * (φ (1.8 Fy) t ε) =  2 * (0.75 * 1.8 * 7200 * 0.1441 * 0.01373 = 38.497 Kips

     

    F max = 2 * Mf / g = 2 * (20 / 0.5) = 80 Kips

    As the flange force does not exceed the maximum, RCnx uses the calculated F value of 38.5 Kips. RAM Connection calculates the maximum flange force acting on the column about either the major or minor axis plus the tension in the in the flange. The user’s model only has data for minor axis calculations. As he noticed, the demand differs when he uses ASD or LFRD and the reason is the calculation has φ as a parameter.

    I hope this helps.



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