Aerospace Engineering > GATE 2011 > Partial Differential Equations
The partial differential equation (PDE) governing free vibrations of a uniform Euler–Bernoulli beam is given by: EI4w/∂x4 + m2w/∂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.
To solve the PDE, the number of boundary conditions (BC) and initial conditions (IC) needed are
A
4 BC, 3 IC
B
2 BC, 2 IC
C
2 BC, 4 IC
D
4 BC, 2 IC

Correct : d

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