A viewing platform in a wild-animal park (Fig. 11-21a) is supported by a row of aluminum pipe columns having a length L = 3.25 m and an outer diameter d = 100 mm The bases of the columns are set in concrete footings, and the tops of the columns are supported laterally by the platform. The columns are being designed to support compressive loads where P = 100 kN.
Determine the minimum required thickness t of the columns (Fig. 11-21b) if a factor of safety n = 3 is required with respect to Euler buckling. (For the aluminum, use 72 GPa for the modulus of elasticity and use 480 MPa for the proportional limit.)
Use a four-step problem-solving approach. Combine steps as needed for an efficient solution.
1, 2. Conceptualize, Categorize:
Critical load: Because of the manner in which the columns are constructed, each column is modeled as a fixed-pinned column (see Fig. 11-20d). Therefore, the critical load is
\quad\quad\quad\quad P_{cr}=\frac{2.046\pi^{2}{{{E I}}}}{{{{L^{2}}}}}\quad\quad (a)
in which I is the moment of inertia of the tubular cross section:
\quad\quad\quad\quad I={\frac{\pi}{64}}[(d^{4}\,-\,\bigl(d\,-\,2t\bigr)^{4}]\quad\quad (b)
Substitute d = 100 mm (or 0.1 m) to get
\quad\quad\quad\quad I =\frac{\pi}{64}[(0.1\,{\bf m})^{4}-(0.1\,{\bf m}-2t)^{4}]\quad\quad(c)
in which t is expressed in meters.
3. Analyze:
Required thickness of the columns: Since the load per column is 100 kN and the factor of safety is 3, each column must be designed for the critical load:
\quad\quad\quad\quad {P}_{cr}=n{P}=3(100\mathrm{kN})=300\mathrm{kN}
Substitute this value for P_{cr} in Eq. (a), and also replace I with its expression from Eq. (c) to obtain
\quad\quad\quad\quad 300\ {\mathrm{kN}}={\frac{2.046\,\pi^{2}(72\,\mathrm{GPa})}{(3.25\,\mathrm{m})^{2}}}\biggl[{\frac{\pi}{64}}\bigl[(0.1\,\mathrm{m})^{4}-(0.1\,\mathrm{m}-2t)^{4}\bigr]\biggr]
Note that all terms in this equation are expressed in units of newtons and meters.
Solve the previous equation to find that the minimum required thickness of the column to meet the specified conditions is
\quad\quad\quad\quad t_{min} = 6.83 ~ mm
4. Finalize:
Supplementary calculations: Knowing the diameter and thickness of the column, now calculate its moment of inertia, cross-sectional area, and radius of gyration. Using the minimum thickness of 6.83 mm gives
\quad\quad\quad\quad I=\frac{\pi}{64}[{d}^{4}-(d-2t)^{4}]=2.18\times10^{6}\mathrm{mm}^{4} \\ \quad\quad A={\frac{\pi}{4}}[d^{2}-(d-2t)^{2}]=1999\,\,{\mathrm{mm}}^{2}\qquad r={\sqrt{\frac{I}{A}}}=33.0\,{\mathrm{mm}}
The slenderness ratio L/r of the column is approximately 98, which is in the customary range for slender columns, and the diameter-to-thickness ratio d/t is approximately 15, which should be adequate to prevent local buckling of the walls of the column.
The critical stress in the column must be less than the proportional limit of the aluminum if the formula for the critical load of Eq. (a) is to be valid. The critical stress is
\quad\quad\quad\quad \sigma_{cr}=\frac{P_{cr}}{A}=\frac{300\,\mathrm{kN}}{1999\,\mathrm{mm}^{2}}=150\,\mathrm{MP}_{\mathrm{a}}
which is less than the proportional limit (480 MPa). Therefore, the calculation for the critical load using the Euler buckling theory is satisfactory.