Thesis-1971-Parthan.pdf (4.75 MB)
Vibration and flutter of unstiffened and orthogonally stiffened circular cylindrical shells
thesis
posted on 2018-07-24, 11:02 authored by S. ParthanThe problem of vibration and flutter analysis of simply-supported unstiffened and orthogonally stiffened
circular cylindrical shells which are typical of missile
bodies has been developed and programmed for digital
computer solution.
An extensive review of the existing literature covering
various aspects of the shell flutter problem is given
with a critical appraisal of the assumptions made, results obtained, etc. A comprehensive chronological bibliography
is also included.
The analysis and the programme which have been developed
are capable of handling shells of arbitrary geometrical,
modal and flow parameters.
In the case of stiffened shells, the stiffener
effects may be treated as 'averaged' ('smeared') or
'discrete' and in each case the influence of eccentricity, in-plane and rotary inertias may be studied.
The aerodynamic generalised forces may be calculated
using the linear piston theory, the linear piston theory
with a correction for curvature, and the exact potential
flow solution.
By combining the invacuo-natural vibration analysis
and the aerodynamic generalised forces the cylindrical
shell flutter problem may be solved and the flutter boundaries
may be obtained in each of the above cases.
The procedures have been illustrated with typical
examples in each of the above cases and the results discussed.
A few shells have been tested using an experimental
vibration rig designed and built for the purpose and compared
with the theoretically predicted invacuo-natural
frequencies and mode shapes.
Funding
Great Britain, Ministry of Technology (contract no.: AT/2170/07/STR).
History
School
- Aeronautical, Automotive, Chemical and Materials Engineering
Department
- Aeronautical and Automotive Engineering
Publisher
© S. ParthanPublisher statement
This work is made available according to the conditions of the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) licence. Full details of this licence are available at: https://creativecommons.org/licenses/by-nc-nd/4.0/Publication date
1971Notes
A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy at Loughborough University.Language
- en