A rolled ISHB 250 section (depth = 250 mm, the width of flange = 250 mm, the thickness of web = 8 .8 mm, the thickness of flange = 9.7 mm) is used to as a compression member. Considering the buckling about the Y-Y axis as per IS 8 00: 2007, the corresponding bu ckling class to which the beam belongs to is:
c
To determine the buckling class of a compression member as per IS 800:2007, we need to consider the type of cross-section, its dimensions, and the axis of buckling. The relevant information for classifying the buckling class of steel sections is provided in Table 10 of IS 800:2007.
The given section is a rolled ISHB 250. The provided dimensions are:
The buckling is considered about the Y-Y axis, which is the major axis for ISHB sections.
According to Table 10 of IS 800:2007, for rolled I-sections buckling about the y-y axis (major axis), the buckling class depends on the ratio of depth to flange width (h/bf) and the thickness of the flange (tf). The criteria are typically:
Let's calculate the ratio of the depth of the section (h) to the width of the flange (bf) for the given ISHB 250 section:
\(\frac{h}{b_f} = \frac{250 \text{ mm}}{250 \text{ mm}} = 1.0\)
The thickness of the flange is tf = 9.7 mm.
We have h/bf = 1.0 and tf = 9.7 mm. We are considering buckling about the Y-Y axis (major axis).
Checking the criteria from IS 800:2007 Table 10 for buckling about the y-y axis:
According to the criteria, if h/bf <= 1.2, the buckling class for a rolled I-section buckling about the y-y axis is 'c'.
Based on the dimensions of the ISHB 250 section and the criteria specified in IS 800:2007 for buckling about the Y-Y axis, the ratio h/bf is 1.0, which is less than or equal to 1.2. Therefore, the corresponding buckling class for this compression member is 'c'.
For a simply supported beam or slab, the effective span is calculated as:
Which of the following is CORRECT for indeterminate beam condition?
A cantilever beam is one which is -
In case of deep beam or in thin webbed R.C.C members, the first crack formed is-
In case of web crippling, the dispersion of load from bearing plate takes place at: