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An experimental investigation of the plastic buckling of aluminum plates /Berrada, Kamal. January 1985 (has links)
No description available.
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The optimal design of laminated plates for maximum buckling load using finite element and analytical methods.Walker, Mark. January 1994 (has links)
In the first part of the study, finite element solutions are presented for the optimal
design of symmetrically laminated rectangular plates subject to a combination of
simply supported, clamped and free boundary conditions. The design objective
is the maximisation of the biaxial buckling load by determining the fibre orientations
optimally with the effects of bending-twisting coupling taken into account.
The finite element method coupled with an optimisation routine is employed in
analysing and optimising the laminated plate designs. The effect of boundary
conditions, the number of layers and bending-twisting coupling on the optimal
ply angles and the buckling load are numerically studied.
Optimal buckling designs of symmetrically laminated rectangular plates under
in-plane uniaxial loads which have a nonuniform distribution along the edges
are presented in the second part of the study. In particular, point loads, partial
uniform loads and nonuniform loads are considered in addition to uniformly distributed
in-plane loads which provide the benchmark solutions. Poisson's effect
is taken into account when in-plane restraints are present along the unloaded
edges. Restraints give rise to in-plane loads at unloaded edges which lead to biaxial
loading, and may cause premature instability. The laminate behavior with
respect to fiber orientation changes significantly in the presence of Poisson's effect
as compared to that of a laminate where this effect is neglected. This change in
behavior has significant implications for design optimisation as the optimal values
of design variables with or without restraints differ substantially. In the present
study, the design objective is the maximisation of the uniaxial buckling load by
optimally determining the fiber orientations. Numerical results, determined using
the finite element method, are given for a number of boundary conditions
and for uniformly and non-uniformly distributed buckling loads.
In the third part of the study, finite element solutions are presented for the optimal
design of symmetrically laminated rectangular plates with central circular
cut-outs subject to a combination of simply supported, clamped and free boundary
conditions. The design objective is the maximisation of the biaxial buckling
load by determining the fiber orientations optimally. The effect of boundary conditions
and bending-twisting coupling on the optimal ply angles and the buckling
load are numerically studied. The results are compared to those for laminates
without holes.
The fourth part of the present study gives optimal designs of symmetrically
laminated angle-ply plates, which are obtained with the objective of maximising
the initial post buckling stiffness. The design involves optimisation over the ply
angles and the stacking sequence to obtain the best laminate configuration. The
stacking sequence is chosen from amongst five candidate designs. It is shown that
the best configuration depends on the ratio of the in-plane loads in the x and y
directions. Results are also given for two additional configurations which do not
exhibit bending-twisting coupling.
The final section of the present study deals with the optimal design of uniaxially
loaded laminated plates subject to elastic in-plane restraints along the unloaded
edges for a maximum combination of prebuckling stiffness, postbuckling
stiffness and buckling load. This multiobjective study illustrates that improved
buckling and post buckling performance can be obtained from plates which are
designed in this fashion. The multiobjective results are also compared to single
objective design results. / Thesis (Ph.D.)-University of Natal, Durban, 1994.
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Single and multiple delamination behavior in composite platesHuang, Haiying 12 1900 (has links)
No description available.
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Geometrically non-linear behaviour of thin-walled members using finite elements.Khan, Abdul Qaseem January 1973 (has links)
No description available.
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An investigation of energy flow through coupled plate structuresSkeen, Michael Berling, Mechanical & Manufacturing Engineering, Faculty of Engineering, UNSW January 2008 (has links)
This PhD thesis presents research aims to improving the dynamic modelling of coupled plate structures across a wide frequency range by using analytical, statistical and experimental methods. The analytical waveguide method is used to model the flexural displacement of coupled plate structures which are simply supported along two parallel edges. A method of quickly predicting the average energy level in a plate from details of the waveguide model is described, and used for comparison with SEA models. The Poynting and Impedance methods of predicting the energy flow in coupled plate structures are investigated. Transmission coefficients for coupled plate structures are evaluated using the analytical waveguide method for both semi-infinite and finite coupled plate structures. Finite transmission coefficients have traditionally been more difficult to evaluate due to the presence of a reverberant field, but in this work a novel method of separating the reverberant field using a scattering matrix method is presented. The transmission coefficients for semi-infinite and finite structures are then compared for L-shaped plates. A modal transmission coefficient is also defined and for the cases considered, and is used to develop an alternative method of deriving the transmission coefficient in a finite structure. Frequency averaged transmission coefficients are also considered, and the transmission coefficients derived for finite and semi-infinite structures are found to be very similar after frequency averaging. Statistical Energy Analysis models of coupled plates are evaluated using transmission coefficients derived from waveguide models. The results of the SEA models are compared to those predicted by the analytical waveguide method. A modal transmission coefficient based SEA model is also investigated. In an attempt to validate the numerical work presented in this thesis, experiments have been conducted. Using a wave extraction technique, both the wave amplitudes and plate properties have been evaluated from experimental data, and are subsequently used to experimentally measure the transmission coefficient for two plates coupled at different angles.
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Linear and geometrically non linear analysis of flat-walled structures by the finite strip method / by C.R.C. Delcourt-BonDelcourt-Bon, Claudine Renee Christine January 1978 (has links)
Typescript (photocopy) / iv, 160 leaves : ill. ; 30 cm. / Title page, contents and abstract only. The complete thesis in print form is available from the University Library. / Thesis (Ph.D.)--University of Adelaide, Dept. of Civil Engineering, 1979
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Flow analysis inside shear and streamlined extrusion dies for feeder plate designAl-Zkeri, Ibrahim A. January 1999 (has links)
Thesis (M.S.)--Ohio University, November, 1999. / Title from PDF t.p.
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Seismic retrofitting of rectangular reinforced concrete columns with partial interaction plating /Wu, Y. F. January 2002 (has links) (PDF)
Thesis (Ph.D.)--University of Adelaide, Dept. of Civil and Environmental Engineering, 2002. / "June 2002" Includes bibliographical references (leaves 349-374).
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Failure analysis of pre-notched composite laminated plates under four-point bending conditions /Arias Gonzales, Sergio. January 1900 (has links)
Thesis (Ph. D.)--Oregon State University, 2009. / Printout. Includes bibliographical references (leaves 140-144). Also available on the World Wide Web.
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An analytical and experimental investigation of active vibration control techniques on coupled plate structures /Keir, John. January 2004 (has links)
Thesis (Ph.D.) - James Cook University, 2004. / Typescript (photocopy) Appendices: leaves 135-137. Bibliography: leaves 126-134.
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