Question 8.15: A tubular column of length l is tapered in wall thickness so......

A tubular column of length l is tapered in wall thickness so that the area and the second moment of area of its cross-section decrease uniformly from A_{1}  and  I_{1} at its center to 0.2A_{1}  and  0.2I_{1} at its ends. Assuming a deflected center-line of parabolic form and taking the more correct form for the bending moment, use the energy method to estimate its critical load when tested between pin-centers, in terms of the preceding data and Young’s modulus E. Hence, show that the saving in weight by using such a column instead of one having the same radius of gyration and constant thickness is about 15 percent.

Answer:       7.01E I_{1}/l^{2}

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The equation for the deflected center line of the column is

\ v={\frac{4\delta}{l^{2}}}z^{2}            (i)

in which δ is the deflection at the ends of the column relative to its center and the origin for z is at the center of the column. Also, the second moment of area of its cross-section varies, from the center to its ends, in accordance with the relationship

I=I_{1}\left(1-1.6{\frac{z}{\overline{{l}}}}\right)          (ii)

At any section of the column the bending moment, M, is given by

M=P_{\mathrm{CR}}(\delta-v)=P_{\mathrm{CR}}\delta\!\left(1-4{\frac{z^{2}}{l^{2}}}\right)          (iii)

Also, from Eq. (i),

{\frac{\mathrm{d}\upsilon}{\mathrm{d}z}}={\frac{8\delta}{l^{2}}}z            (iv)

Substituting in Eq. (8.47) for M, I, and dυ/dz,

U+V=\int_{0}^{l}\!\frac{M^{2}}{2E I}\ \mathrm{d}z-\frac{P_{\mathrm{CR}}}{2}\int_{0}^{l}\!\left(\frac{\mathrm{d}\nu}{\mathrm{d}z}\right)^{2}\!\mathrm{d}z          (8.47)

 

U+V=2\int_{0}^{l/2}{\frac{P_{\mathrm{CR}}^{2}\delta^{2}(1-4z^{2}/l^{2})^{2}}{2E I_{1}(1-1.6z/l)}}\mathrm{d}z-{\frac{P_{\mathrm{CR}}}{2}}2\int_{0}^{l/2}{\frac{64\delta^{2}}{l^{4}}}z^{2}\mathrm{d}z

or

U+V={\frac{P_{\mathrm{CR}}^{2}\delta^{2}}{E I_{1}l^{3}}}\int_{0}^{l/2}{{\frac{(l^{2}-4z^{2})^{2}}{l-1.6z}}\mathrm{d}z-{\frac{64P_{\mathrm{CR}}\delta^{2}}{l^{4}}}} \int_{0}^{l/2}{z^{2}dz}           (v)

Dividing the numerator by the denominator in the first integral in Eq. (v) gives

U+V={\frac{P_{\mathrm{{CR}}}^{2}\delta^{2}}{E I_{1}l^{3}}}\left[\int_{0}^{l/2}{(-10z^{3}-6.25l z^{2}+1.09l^{2}z+0.683l^{3})\mathrm{d}z}+0.317l^{3}\int_{0}^{l/2}{\frac{\mathrm{d}z}{(1-1.6z/l)}} \right] -{\frac{64P_{\mathrm{CR}}\delta^{2}}{l^{4}}}\bigg[{\frac{z^{3}}{3}}\bigg]^{l/2}

Hence,

U+V={\frac{P_{\mathrm{CR}}^{2}\delta^{2}}{E I_{1}l^{3}}}\left[-10\frac{z^{4}}{4}-6.25l\frac{z^{3}}{3}+1.09l^{2}\frac{z^{2}}{2}+0.683l^{3}z-\frac{0.317}{1.6}l^{4}\log_{e}\left(1-\frac{1.6z}{l}\right)\right] _{0}^{l/2}-{\frac{8P_{\mathrm{CR}}\delta^{2}}{3l}}

i.e.,

U+V=\frac{0.3803P_{\mathrm{CR}}^{2}\delta^{2}l}{E I_{1}}-\frac{8P_{\mathrm{CR}}\delta^{2}}{3l}

From the principle of the stationary value of the total potential energy,

\frac{\partial(U+V)}{\partial\delta}=\frac{0.7606P_{\mathrm{CR}}^{2}\delta l}{E I_{1}}-\frac{16P_{\mathrm{CR}}\delta}{3l}=0

Hence,

P_{\mathrm{CR}}={\frac{7.01E I_{1}}{l^{2}}}

For a column of constant thickness and second moment of area I_{2},

P_{\mathrm{CR}}={\frac{\pi^{2}E I_{2}}{l^{2}}}   ((see Eq.(8.5))

 

P_{\mathrm{CR}}={\frac{\pi^{2}E I}{l^{2}}}          (8.5)

For the columns to have the same buckling load,

{\frac{\pi^{2}E I_{2}}{l^{2}}}={\frac{7.01E I_{1}}{l^{2}}}

so that

I_{2}=0.7I_{1}

Thus, since the radii of gyration are the same,

A_{2}=0.7A_{1}

Therefore, the weight of the constant thickness column is equal to \rho A_{2}l=0.7\rho A_{1}l. The weight of the tapered column = \rho\times\mathrm{average~thickness}\times l=\rho\times 0.64 A_{1}\;l.

Hence the saving in weight = 0.7\rho A_{1}l-0.6\rho A_{1}l=0.1~\rho A_{1}~l.

Expressed as a percentage,

\mathrm{swing~in~weight}=\frac{0.1/\rho A_{1}l}{0.7\rho A_{1}l}\times100=14.3%

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