A column has a solid circular cross section, 1.25 inches in diameter; it has a length of 4.50 ft and is pinned at both ends. If it is made from AISI 1020 cold-drawn steel, what would be a safe column loading?
A column has a solid circular cross section, 1.25 inches in diameter; it has a length of 4.50 ft and is pinned at both ends. If it is made from AISI 1020 cold-drawn steel, what would be a safe column loading?
Objective Specify a safe loading for the column.
Given Solid circular cross section: diameter = d = 1.25 in; length = L = 4.50 ft. Both ends of the column are pinned.
Material: AISI 1020 cold-drawn steel.
Analysis Use the procedure in Figure 6-4.
Results Step 1. For the pinned-end column, the end-fixity factor is K = 1.0. The effective length equals the actual length; KL = 4.50 ft = 54.0 in.
Step 2. From Appendix 1, for a solid round section,
APPENDIX 1 PROPERTIES OF AREAS | |
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A = \pi D^4/4 r= D/4 I = \pi D^4/64 J = \pi D^4/32 S = \pi D^3/32 Z_p =\pi D^3/16 |
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A = \pi (D^2 – d^2)/4 r = \sqrt{D^2 + d^2} /4 I = \pi (D^4 – d^4)/64 J = \pi (D^4 – d^4)/32 S = \pi (D^4 – d^4)/32D Z_p =\pi (D^4 – d^4)/16D |
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A = S^2 r = s/\sqrt{12} I= 5^4/12 S = 5^3/6 |
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A = BH r_x = H/\sqrt{12} I_x = BH^3/12 r_y = B/\sqrt{12} S_x = BH^2/6 |
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A = BH /2 r = H/\sqrt{18} I = BH^3/36 S = BH^2/24 |
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A =\pi D^2/8 r= 0.132D I = 0.007D^4 S = 0.024D^3 |
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A = 0.866D^2 r = 0.264D I = 0.06D^4 S= 0.12D^3 |
A = area I = moment of inertia S = section modulus r = radius of gyration = \sqrt{I/A} J = polar moment of inertia Z_p = polar section modulus |
r = D/4 = 1.25/4 = 0.3125 in
Step 3. Compute the slenderness ratio:
\frac{KL}{r} =\frac{1.0(54)}{0.3125}= 173
Step 4. Compute the column constant from Equation (6-4). For AISI 1020 cold-drawn steel, the yield strength is 51 000 psi. and the modulus of elasticity is 30 ×10^6 psi. Then
C_c=\sqrt{\frac{2\pi ^2E}{s_y}} =\sqrt{\frac{2\pi ^2(30\times 10^6)}{51000}} = 108
Step 5. Because KL/r is greater than C_c, the column is long, and Euler’s formula should be used. The area is
A=\frac{\pi D^2}{4} =\frac{\pi (1.25)^2}{4}=1.23 \ in^2
Then the critical load is
P_{cr}=\frac{\pi ^2EA}{(KL/r)^2}=\frac{\pi ^2(30\times 10^6) (1.23)}{(173)^2}=12 200 lb
At this load, the column should just begin to buckle. A safe load would be a reduced value, found by applying the design factor to the critical load. Let’s use N= 3 to compute the allowable load, P_a = (12 200)/3=4067 lb
Comment The safe load on the column is 4067 lb.