Aerospace Engineering > GATE 2011 > Beam Boundary Conditions
The partial differential equation (PDE) governing free vibrations of a uniform Euler–Bernoulli beam is given by:
EI ∂4w/∂x4 + m ∂2w/∂t2 = 0,
where EI is the flexural stiffness, m is the mass per unit length, w(x, t) is the bending displacement,
x is the coordinate along the beam length, t is time, and L is the beam length.
For the cantilever beam shown in the figure, which of the following CANNOT be a possible
boundary condition?
boundary condition?
Correct : c
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