Given an AISC column member determine the following when the member is loaded as shown and fill in the blanks below.

Compute the column's effective slenderness ratio. $($Round to the nearest two decimal places$)$

What maximum $($critical$)$ load can the member take before buckling would be expected?

Compute the allowable load on the column for a given design factor of N$.$

The member is made from ASTM A$500$ Grade B material.

The AISC member shape, column end condition, load and dimensions are listed below.

All answers are in SAE units.

QB$\_$Final Problem$6$ textbook image.png

QB$\_$Final Problem$6$ column image.png

Member Shape and Material:

Length L $=20\mathrm{.}00$ ft

End A Pin

End B Pin

N $=2\mathrm{.}50$

Member $=$ HSS$10$x$4$x$\mathrm{.}125$

$7\mathrm{.}1.$ Compute the columns effective slenderness ratio. $=$

$7\mathrm{.}2.$ What maximum load can the member take before buckling would be expected in lbf$?=$

$7\mathrm{.}3.$ Compute the allowable load on the column for a given design factor of N in lbf$.=$Given an AISC column member determine the following when the member is laaded as

shown and fill in the blonks below.

Compute the column's effective slenderness ratia. $($Round to the nearest two decimal

places$]$

What maximum $($critical$)$ lood can the member take before buckling would be expected?

Compute the allowable lood on the column for a given design factor of $N.$

The member is mode from ASTM A$500$ Grade B material.

The AISC member shape, column end condition, lood and dimensions are fisted below.

AN answers are in SAE units.

AISC Structural

Member

End $A$

End $B$

Member Shape and Moterial:

Length L $=20\mathrm{.}00ft$

End A Pin

End B Pin

$N=2\mathrm{.}50$

Member $=$ H$5510$x$4$x$.125$

$7\mathrm{.}1.$ Compute the calumns effective slenderness ratio. $-$

$7\mathrm{.}2.$ What maximum load can the member take before budkling would be expected in Ibf? $-$

$7\mathrm{.}3.$ Compute the allowable lasd on the column for a given design foctor of $N$ in lbf$.-$