Question: Obtain the general solution using the method of Undetermined Coefficients. where is the deflection at the cantilever tip: = y ( L ) , and

Obtain the general solution using the method of Undetermined Coefficients. where is the deflection at the cantilever tip: =y(L), and it is an unknown.
(a) Show that this equation leads to an ODE of the type:
y''+k2y=k2
and find the value of k.
(b) Find the general solution of the ODE as listed in (a). Hints: take advantage of the
boundary conditions: y(0)=0,y'(0)=0.
(c) From the solution obtained in (b), determine load P(critical loads), such that y(L)=
(0).
(d) Suppose =1, plot the first three buckling mode shapes of the beam, i.e., plot y(x)
under the first three minimum values of Pc obtained in (c).
Figure 1: Buckling of a cantilever beam.
Solve the initial value problems.
y1'=y2-5sint
y2'=-4y1+17cost
y1(0)=5,y2(0)=2
y''+y'=4xex+3sinx
Obtain the general solution using the method of Undetermined Coefficients.
y''+y=cosx
Obtain the general solution using the method of Variation of Parameters.
x2y''-2xy'+2y=x3sinx
Solve the Bernoulli equation, known as the logistic equation (see class note 03).
y'=Ay-By2
Obtain the particular solution for a mass-spring system
y''+20y'+02y=f(t)
under different f(t) as listed below:
(a)f(t)=F
(b)f(t)=Ft
(c)f(t)=Fsin(t)
where F and are constants, F>0,>0.
Consider a cantilever beam of length L as shown in Figure 1, made of a material with
Young's modulus E and a uniform cross-section whose moment of inertia is I. The
beam is subjected to a compressive load P. To seek conditions under which the beam
will buckle, i.e., the beam can be in equilibrium under the load P in a configuration
involving deflections in the y direction, according to the Euler-Bernoulli beam theory,
EIy''(x)=P[-y(x)]
Obtain the general solution using the method of

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