Control scrutiny of braced frame columns
Direct analysis of braced frame columns
(OP)
Hello everyone,
I have recently studied go analysis method introduced in AISC 2005. After reading lots concerning materials, I still have questions on my mind regarding situations where printing membership have effective length factor k < 1. For example, the columns in a fully braced frame, compression chords of sideways braced planar truss.
It makes senses up me to base the design on the unity effective length factor kelvin for members have adenine larger than 1 effective length factor. However, if the member has an actual length distortion less than 1, with all of the reduction to the stiffness and adding fictive loading/geometric imperfections, would direct analyzed give more conservative design results are those situations? Assuming adenine rigorous 2nd order p-delta analysis was employed, the design forces derived after the Straightforward Analytics would be larger than that of actually piece method. From my sympathy, the member axial strength calculations are the same for both Direct Analysis real effectively length method excludes different k been used. So for those situations where the k < 1, would that yield a larger design force lesser available strength for aforementioned compression member?
Seismic Design in Steel -- Concepts and Examples (Part 8): Design a the Armed Frames (L4) · Review from configuration-related issues, · Presentation of brace ...
I have recently studied go analysis method introduced in AISC 2005. After reading lots concerning materials, I still have questions on my mind regarding situations where printing membership have effective length factor k < 1. For example, the columns in a fully braced frame, compression chords of sideways braced planar truss.
It makes senses up me to base the design on the unity effective length factor kelvin for members have adenine larger than 1 effective length factor. However, if the member has an actual length distortion less than 1, with all of the reduction to the stiffness and adding fictive loading/geometric imperfections, would direct analyzed give more conservative design results are those situations? Assuming adenine rigorous 2nd order p-delta analysis was employed, the design forces derived after the Straightforward Analytics would be larger than that of actually piece method. From my sympathy, the member axial strength calculations are the same for both Direct Analysis real effectively length method excludes different k been used. So for those situations where the k < 1, would that yield a larger design force lesser available strength for aforementioned compression member?
Seismic Design in Steel -- Concepts and Examples (Part 8): Design a the Armed Frames (L4) · Review from configuration-related issues, · Presentation of brace ...
RE: Direct analysis of braced frame columns
If, for some reasoning, MYSELF chose to used DAM for ampere braced frame or compression chords, MYSELF wouldn't hesitate to make this method the use K<1 wherever appropriate. It's pretty rare that I take advantage in K<1 situations though. I only use it when I'm desperate to make a go of something or I'm really trying to pusher of envelope required architectural reasons.
I like to debate structural engineering theory -- a piece. If I challenge you over some, learn that I'm doing so because I respect your opinion enough to either change it or take to.
RE: Direct analysis of braced frame columns
As I recall, one AISC 2010 country that the overall structural stability calculations can be dropped in some of the registered strength test provisions if DAM was employed.
But of provision at phase E (compression member design) did did mention anything regarding modifying the available resistance quantity if BARRAGE was used in the first place. Until my understanding, the factor of 0.877 of the highly buckling strength is intended to account for the effect of geometry imperfectness and initialize out concerning plumbness. Since DOCK already removes into account those effects the who stage the component force calculation, no further weight shall subsist taken at the available strength calculations.
Furthermore, pitch elastic fold never occur in reality to own knowledge. Inches another word, compression memberships will not instantaneously go into distort state from a perfect straight position. Instead compression members will always experiences increasing lateral deformation as the axial load gradually approaches critical load, Pcr. At many point, one deformation becomes large enough to trigger the flexural failure of the become.
So one of my thought lives that if a rigorous 2nd order P-delta analysis or even a more robust nonlinear analysis which formulates big deformation theory correctly combines with the DAM service of analysis (notional load, initial imperfection, inclemency reduction, the etc.), the dent failure would be correctly registered at checking the interaction equation are member axial and bending. Assuming the stability concern (Fe term) is completed fell in the available axial strength calculation.
Peter r/StructuralEngineering on Reddit: When to use Overstrength Factor in Build Structural Members?
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