Specify a suitable diameter of a solid, round cross section for a machine link if it is to carry 9800 lb of axial compressive load. The length will be 25 in, and the ends will be pinned.Use a design factor of 3.Use AISI 1020 hot-rolled steel.
Specify a suitable diameter of a solid, round cross section for a machine link if it is to carry 9800 lb of axial compressive load. The length will be 25 in, and the ends will be pinned.Use a design factor of 3.Use AISI 1020 hot-rolled steel.
Objective Specify a suitable diameter for the column.
Given solid circular cross section: L = 25 in; use N = 3.Both ends are pinned.Material: AISI 1020 hot-rolled steel.
Analysis Use the procedure in Figure 6_13. Assume first that the column is long.
Results From Equation (6_9),D=\left[\frac{64 N P_{a}(K L)^{2}}{\pi^{3} E}\right]^{1 / 4}
D=\left[\frac{64 N P_{a}(K L)^{2}}{\pi^{3} E}\right]^{1 / 4}=\left[\frac{64(3)(9800)(25)^{2}}{\pi^{3}\left(30 \times 10^{6}\right)}\right]^{1 / 4}
D=1.06 in
The radius of gyration can now be found:r=D / 4=1.06 / 4=0.265 \mathrm{in} The slenderness ratio is K L / r=[(1.0)(25)] / 0.265=94.3 For the AISI 1020 hot-rolled steel,s_{y}= 30 000 psi. The graph in Figure 6_5 showsC_{c}to be approximately 138. Thus, the actual KL/r is less than the transition value, and the column must be redesigned as a short column, using Equation (6_10) derived from the Johnson formula:D=\left[\frac{4 N P_{a}}{\pi s_{y}}+\frac{4 s_{y}(K L)^{2}}{\pi^{2} E}\right]^{1 / 2}
(6_10)
D=\left[\frac{4(3)(9800)}{(\pi)(30000)}+\frac{4(30000)(25)^{2}}{\pi^{2}\left(30 \times 10^{6}\right)}\right]^{1 / 2}=1.23 \mathrm{in}Checking the slenderness ratio again, we have K L / r=[(1.0)(25)] /(1.23 / 4)=81.3
Comments This is still less than the transition value, so our analysis is acceptable. A preferred size of D = 1.25 in could be specified.An alternate method of using spreadsheets to design columns is to use an analysis approach similar to that shown in Figure 6_9 but to use it as a convenient “trial and error”tool. You could compute data by hand, or you could look them up in a table for A,I, and r for any desired cross-sectional shape and dimensions and insert the values into the spreadsheet. Then you could compare the computed allowable load with the required value and choose smaller or larger sections to bring the computed value close to the required value. Many iterations could be completed in a short amount of time. For shapes that allow computing r and A fairly simply, you could add a new section to the spreadsheet to calculate these values. An example is shown in Figure 6_14, where the differently shaded box shows the calculations for the properties of a round cross section. The data are from Example Problem 6_3, and the result shown was arrived at with only four iterations.