Question 8.4: Determine the equation of the deflection curve for a cantile...
Determine the equation of the deflection curve for a cantilever beam AB supporting a triangularly distributed load of maximum intensity q_0 (Fig. 8-14a).
Also, determine the deflection \delta_B and angle of rotation \theta_B at the free end (Fig. 8-14b). Use the fourth-order differential equation of the deflection curve (the load equation). (Note: The beam has length L and constant flexural rigidity EI.)

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Differential equation of the deflection curve. The intensity of the distributed load is given by the following equation (see Fig. 8-14a):
q=\frac{q_0(L-x)}{L} (8-40)
Consequently, the fourth-order differential equation (Eq. 8-12c) becomes
EIv''''=-q (8-12c)
=-\frac{q_0(L-x)}{L} (a)
Shear force in the beam. The first integration of Eq. (a) gives
EIv'''=\frac{q_0}{2L} (L-x)^2+C_1 (b)
The right-hand side of this equation represents the shear force V (see Eq. 8-12b). Because the shear force is zero at x = L, we have the following boundary condition:
EIv''' = V (8-12b)
v'''(L) = 0
Using this condition with Eq. (b), we get C_1 = 0. Therefore, Eq. (b) simplifies to
EIv'''=\frac{q_0}{2L} (L-x)^2 (c)
and the shear force in the beam is
V=EIv'''=\frac{q_0}{2L} (L-x)^2 (8-41)
Bending moment in the beam. Integrating a second time, we obtain the following equation from Eq. (c):
EIv''=-\frac{q_0}{6L} (L-x)^3+C_2 (d)
This equation is equal to the bending moment M (see Eq. 8-12a). Since the bending moment is zero at the free end of the beam, we have the following boundary condition:
EIv'' = M (8-12a)
v''(L) = 0
Applying this condition to Eq. (d), we obtain C_2 = 0, and therefore the bending moment is
M=EIv''=-\frac{q_0}{6L} (L-x)^3 (8-42)
Slope and deflection of the beam. The third and fourth integrations yield
EIv'=\frac{q_0}{24L} (L-x)^4+C_3 (e)
EIv=-\frac{q_0}{120L} (L-x)^5+C_3x+C_4 (f)
The boundary conditions at the fixed support, where both the slope and deflection equal zero, are
v'(0) = 0 v(0) = 0
Applying these conditions to Eqs. (e) and (f), respectively, we find
C_3=-\frac{q_0L^3}{24} C_4=\frac{q_0L^4}{120}
Substituting these expressions for the constants into Eqs. (e) and (f ), we obtain the following equations for the slope and deflection of the beam:
v'=-\frac{q_0x}{24LEI} (4L^3-6L^2x+4Lx^2-x^3) (8-43)
v=-\frac{q_0x^2}{120LEI} (10L^3-10L^2x+5Lx^2-x^3) (8-44)
Angle of rotation and deflection at the free end of the beam. The angle of rotation \theta_B and deflection \delta_B at the free end of the beam (Fig. 8-14b) are obtained from Eqs. (8-43) and (8-44), respectively, by substituting x = L. The results are
\theta _B=-v'(L)=\frac{q_0L^3}{24EI} \delta _B=-v(L)=\frac{q_0L^4}{30EI} (8-45 a,b)
Thus, we have determined the required slopes and deflections of the beam by solving the fourth-order differential equation of the deflection curve.