Question 5.6: A stiffening ring is placed around a cylinder at a distance ...

A stiffening ring is placed around a cylinder at a distance from the ends as shown in Figure 5.12. The cylinder has a radius of 50.0 in. and a thickness of 0.25 in. and is subjected to an internal pressure of 100 psi.
Assuming E=30 \times 10^{6} psi and \mu=0.3, find
a) The discontinuity stress in the shell with the ring assumed to have infinite rigidity.
b) The discontinuity stress in the shell and ring if the ring has a thickness of 0.375 in. and a depth of 4.0 in.

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A free-body diagram of the shell-to-ring junction is shown in Figure 5.13. Because the ring is assumed to have infinite rigidity, the deflection due to pressure must be brought back to zero by a force Q_{0}. Also, because the slope at the shell-to-ring junction is zero (due to symmetry), a moment M_{0} must be applied at the junction to reduce the slope created by force Q_{0} to zero. From Figure 5.13,

deflection due to P − deflection due to Q_{0} + deflection due to M_{0} = 0.

The deflection due to P is obtained from Eq. (1) in Example 5.5, whereas the deflections due to M_{0} and Q_{0} are obtained from Eq. (5.24). Hence,

w=\frac{P r^{2}}{E t}\left(1-\frac{\mu}{2}\right)                        Eq. (1)

\frac{ d ^{3} w}{ d x^{3}}=\frac{-1}{D}\left(2 \beta M_{0} D_{\beta x}-Q_{0} B_{\beta x}\right)                          (5.24)

\frac{P r^{2}}{E t}\left(1-\frac{\mu}{2}\right)-\frac{Q_{0}}{2 \beta^{3} D}+\frac{M_{0}}{2 \beta^{2} D}=0

From Eq. (5.15),

D=\frac{E t^{3}}{12\left(1-\mu^{2}\right)}                     (5.15)

D = 0.00143E,

and from Eq. (5.20),

\beta^{4}=\frac{E t}{4 r^{2} D}=\frac{3\left(1-\mu^{2}\right)}{r^{2} t^{2}}                                    (5.20)

\beta=0.3636

Hence, the deflection compatibility equation becomes

M_{0}-2.750 Q_{0}=-321.39                       (1)

The second compatibility equation gives

rotation due to Q_{0} − rotation due to M_{0} = 0

or

Q_{0}-2 \beta M_{0}=0                              (2)

Solving Eqs. (1) and (2) gives

M_{0}=321.4 \text { in. }- lb / \text { in }

The maximum longitudinal stress is given by

\sigma_{x}=\frac{Pr}{2 t}+\frac{6 M_{0}}{t^{2}}

= 40,900 psi.

The maximum hoop moment is given by Eq. (5.17) as

M_{\theta}=\mu M_{x}                                  (5.17)

M_{\theta}=96.4 \text { in. -lb } / \text { in. }

The hoop force N_{\theta} is given by Eq. (5.19) as

N_{\theta}=\frac{-E t w}{r}                                      (5.19)

N_{\theta}=\frac{E t w}{r}

But because w=0, N_{\theta} is equal to zero and the maximum hoop stress is

\sigma_{\theta}=\frac{6 M_{\theta}}{t^{2}}

= 9300 psi.

 

Solution (b):

The shell deformations are expressed as follows:

Due to P

w=\frac{Pr^{2}}{E t}\left(1-\frac{\mu}{2}\right)

 

\theta=0

 

Due to Q_{0}

 

w=\frac{Q_{0}}{2 \beta^{3} D}

 

\theta=\frac{-Q_{0}}{2 \beta^{2} D}

Due to M_{0},

w=\frac{M_{0}}{2 \beta^{2} D}

 

\theta=\frac{M_{0}}{\beta D}

The ring deformations are expressed as follows:

Due to P,

w=\frac{Pr(r+d / 2)}{d E}

 

\theta=0

Due to Q_{0},

w=\frac{2 Q_{0} r(r+2)}{b d E}

 

\theta=0

Due to M_{0},

w = 0

\theta=0

The deflection compatibility is

\left[w_{ p }-w_{Q_{0}}+w_{M_{0}}\right]_{ cyl }=\left[w_{ p }+w_{2 Q_{0}}\right]_{\text {ring }}

 

\frac{P r^{2}}{E t}\left(1-\frac{\mu}{2}\right)-\frac{Q_{0}}{2 \beta^{3} D}+\frac{M_{0}}{2 \beta^{2} D}=\frac{P_{ r }(r+d / 2)}{d E}

 

+\frac{2 Q_{0}(r+d / 2)}{b d E}

Or

M_{0}-4.06 Q_{0}=-296.8                          (3)

Similarly,

\left[\theta_{ p }+\theta_{M_{0}}-\theta_{Q_{0}}\right]_{ cyl }=\left[\theta_{ p }+\theta_{M_{0}}-\theta_{Q_{0}}\right]_{\text {ring }}

Or

\frac{M_{0}}{\beta D}-\frac{Q_{0}}{2 \beta^{2} D}=0

And

2 \beta M_{0}-Q_{0}=0                           (4)

Solving Eqs. (3) and (4) yields

M_{0} = 152.0 in.-lb / in

Q_{0} = 110.6 lb /in.

The hoop stress in the ring is

\sigma_{ r }=\frac{Pr}{d}+\frac{2 Q_{0} r}{b d}

= 1250 + 7370

= 8620 psi.

The maximum longitudinal stress in the cylinder is

\sigma_{x}=\frac{P r}{2 t}+\frac{6 M_{0}}{t^{2}}

 

=\frac{100 \times 50}{2 \times 0.25} \times \frac{6 \times 152}{(0.25)^{2}}

= 24,600 psi.

The hoop force at the discontinuity is

N_{\theta}=\frac{E t w}{r}

Where

w=w_{ p }-w_{Q_{0}}+w_{M_{0}}

 

=\frac{P r^{2}}{E t}\left(1-\frac{\mu}{2}\right)-\frac{Q_{0}}{2 \beta^{3} D}+\frac{M_{0}}{2 \beta^{2} D}

 

=\frac{447,500}{E}

Or

N_{\theta}=\frac{E(0.25)(447,500 / E)}{50}

= 2238lb /in.,

and the hoop stress at the discontinuity is

\sigma_{\theta}=\frac{N_{\theta}}{t}+\frac{6 M_{\theta}}{t^{2}}

 

=\frac{2238}{0.25}+\frac{6(0.3 \times 152)}{0.25^{2}}

= 13,300 psi,

whereas away from discontinuity,

\sigma_{\theta}=\frac{P r}{t}=20,000 psi
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