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This thesis is an attempt to study some of the problems
of flexural vibrations of beams and plates and is divided into
two parts. The first part deals with problems relating to the
flexural vibrations of uniform beams and naturally curved rods
which include th effects of rotatory inertia and shear. The
equations for flexural vibrations of a uniform cantilever beam
according to Timoshenko theory have been numerically solved and
it is shown that results similar to those of Anderson for a beam
supported at both ends can be obtained. The equations of flexural
vibrations of a deep beam obtained by a method of successive
approximations are studied and solved for the case of a cantilever
beam for various ratios of cepth to length. These are compared
with the solution of Timoshenko's equation for the same beam.
Here we include the effects of shear and rotatory inertia, but do
not assume that the cross-sections of the beam remains plane as
assumed by Timoshenko.
For naturally curved elastic rods, the equations f0r
flexural vibrations given by Morley, where the neutral axis forms
a plane curve of constant radius, is worked out. The effects of
rotatory inertia and shear are included in the same way as in
Timoshenko theory for straight rods and the effect of the extension
of the neutral axis is also included. Numerical solutions for a
rod fixed at both ends are obtained for rods of different
curvatures and compared with the results for a straight uniform
beam. The equations of vibrations of a short thin arch in the
shape of catenary are also derived, the displacements being
confined to the plane of the catenary. Numerical solutions of
ii
the equations for the symmetrical case of fundamental mode of
vibration are obtained. These equations and their solutions
would be of significance in the study of vibrations of the 325
feet-span concrete shell arch designed and constructed at the
University of Roorkee. •
In the second part a method of successive approximations
is presented to obtain the vibrations equations of an Isotropic
elastic plate under conditions which are more general than those
of Timoshenko theory. Here, we include the secondary effects of
rotatory inertia and shear, but do not assume that the displace
ments follow a linear law as was done by Timoshenko or Mindlin.
The governing equations for the flexural vibrations of plates
are solved•separately for square and circular plates for various
ratios of thickness to the sice or diameter of the respective
plates. Solutions are also given of the equations for flexural
vibrations of isotropic elastic plates according to Minclin's
theory for the case of simply supported uniformly loaded thin
square and circular plates and the comparison is ^a6e between the
results of two equations. The former method of analysis yields
results more accurate than those by the existing methods. The
method therefore offers a means of solving vibrational problems
to a high degree of accuracy. Lastly an attempt has been made to
make a comparative study of the equation derived by the method
of successive approximations with the exact theory, Mindlin1s
theory and Lagrange's classical plate theory through the results
for the case of straight crested waves.
The contents of each chapter are outlined below.
iii
FART I. Chapter I. The equations for flexural vibrations of a
uniform beam according to Timoshenko theory are studied and
numerically solved for the case of a cantilever beam for various
slenderness ratios.
Chapter II. A method of successive approximations to derive the
equation for flexural vibrations of a deep beam is studied. The
equation is then solved numerically for the case of a cantilever
beau for various values of depth to lengtn ratios.
Charter III. Morley's equations for flexural vibrations of a
naturally curved elastic rod are obtained and solutions are given
for the case of a rod fixed at both ends for various curvatures.
Chapter IV. The equations of vibrations of a short thin arch
in the shape of catenary are derived and solved for the symaetrical
case of the fundamental mode of vibration.
PART II. Chapter V. A equation for flexural vibrations of an
isotropic elastic plate is derived by the method of successive
approximations.
Chapter VI. The equation of the above chapter has been solved
for the case of a simply suppored thin square plate.
Chapter VII. The equation of the chapter V has been solved for
another case of a simply supported thin circular plate.
Chapter VIII. Minclin's equation for flexural vibrations of
isotropic elastic plates is obtained and a numerical solution is
given for the case of a simply supported thin square plate.
Chapter IX. The equation of the above chapter has been solved for
another case of a simply supported thin circular plate.
iv
Chapter X. In this concluding chapter, an attempt has been
made to make a comparative study of the equation derived by the
method of successive approximations in Chapter V with the exact
theory, Mindlin's theory and Lagrange's Classical plate theory
through the resiilts for tke case of strajgit crested waves.
The work, presented here, is original research by the
author except sections 1.1, 2.1, 3,2 and 8.2 which have been put
in to present a connected account of the whole. The material
of Chapters I,VI ana IX is being published in the Bulletins of
Calcutta Mathematical Society. The Chapters V and VIII are
published in the proceedings of National Institute of Sciences of
India and Chapter VII in the University of Roorkee Research
Journal. The material of Chapter IV was presented in the second
symposium of Earthquake Engineering held at Roorkee in December,
1962. |
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