Question 8.8: A long strut AB of length L is of uniform section throughout...
A long strut AB of length L is of uniform section throughout. A thrust P is applied at the ends eccentrically, on the same side of the centre line with eccentricity at the end B twice than that at the end A. Show that the maximum bending moment occurs at a distance x from end A, where
tanλx=sinλL2−cosλL and λ=EIP
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Assuming the column to be fundamental one (i.e., pinned at both ends) with eccentric load at both ends, we show the schematic structural diagram of the column in Figure 8.21(a).
In Figure 8.21(a), we represent the eccentricity at ends A and B as ε and 2ε, respectively. In Figure 8.21(b), we represent the free-body diagram of the entire column while in Figure 8.21(c), we show the free-body diagram of the column of a section cut out at a distance x (0 ≤ x ≤ L) from end A. In Figure 8.21(c), axial force Nx, shear force Vx and bending moment Mx are shown in their positive senses.
Now, from Figure 8.21(b), for equilibrium ( note ΣFx=0 and ΣFy=0 have automatically been satisfied), we must have:
∑Mz=0⇒QL=Pε
or Q=LPε (1)
Again from Figure 8.21(c):
∑Mz=0⇒Mx=Pε+Py+Qx
where y is the depression of the column at a distance x from end A [as shown in Figure 8.21(b) above].
Therefore, from flexure equation:
(EI)dx2d2y=−Mx=−Py−Qx−Pε
or dx2d2y=⎩⎪⎧−EIP⎭⎪⎫y−⎩⎪⎧EIQ⎭⎪⎫x−(EIP)ε
or dx2d2y+λ2y=−λ2ε−λ2PQx( where λ2=P/EI)
or dx2d2y+λ2y=−λ2⎩⎪⎧PQx+ε⎭⎪⎫ (2)
Clearly, the above is a second-order non-homogeneous linear differential equation and will have complementary function and particular integral as its solution components. Therefore,
y=(A1cosλx+A2sinλx)−(PQx+ε) (3)
where A1 and A2 are the two arbitrary constants to be determined from the geometric boundary conditions of the problem. Obviously, we have at x = 0, y = 0 and at x = L, y = 0. Thus, from Eq. (3), we get
A1−ε=0⇒A1=ε (4)
and εcosλL+A2sinλL−PQL−ε=0
But from Eq. (1), QL/P = ε. Thus, the above expression becomes
εcosλL+A2sinλL−2ε=0
A2=sinλLε(2−cosλL) (5)
Now, from Eq. (3), we obtain
y=ε[cosλx+⎩⎪⎧sinλL2−cosλL⎭⎪⎫sinλx−Lx−1] (6)
This is the equation of the elastic line of the column. Now, bending moment at any distance x is
Mx=Py+Pε+Qx
or Mx=P[y+ε+Lεx] [as QL = Pε by Eq. (1)]
Putting expression of y from Eq. (6) above, we get
Mx=Pε[cosλx+⎩⎪⎧sinλL2−cosλL⎭⎪⎫sinλx] (7)
For Mx to be maximum, clearly cosλx+[(2–cosλL)/sinλL]sinλx is to be maximum, that is, when
dxd{cosλx+(sinλL2−cosλL)sinλx}=0
or −sinλx+(sinλL2−cosλL)cosλx=0
or tanλx=⎩⎪⎧sinλL2−cosλL⎭⎪⎫ (where λ2=P/EI )
Alternative Solution: Let (2 – cosλL)/sinλL = p. Now,
cosλx+⎩⎪⎪⎧sinλL2−cosλL⎭⎪⎪⎫sinλx=cosλx+psinλx=1+p2sin(λx+θ)
where tan θ= 1/p. Therefore, cosλ x + p sinλ x is maximum, that is, 1 when
λx+θ=2π
or λx=2π−θ
or tanλx=cotθ=p=sinλL2−cosλL (as before)
