Citation
Kosecoff, Michael Alan (1975) Some Problems in Nonlinear Elasticity. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/KYF4PD11. https://resolver.caltech.edu/CaltechTHESIS:03292013141424985
Abstract
Two separate problems are discussed: axisymmetric equilibrium configurations of a circular membrane under pressure and subject to thrust along its edge, and the buckling of a circular cylindrical shell.
An ordinary differential equation governing the circular membrane is imbedded in a family of ndimensional nonlinear equations. Phase plane methods are used to examine the number of solutions corresponding to a parameter which generalizes the thrust, as well as other parameters determining the shape of the nonlinearity and the undeformed shape of the membrane. It is found that in any number of dimensions there exists a value of the generalized thrust for which a countable infinity of solutions exist if some of the remaining parameters are made sufficiently large. Criteria describing the number of solutions in other cases are also given.
Donnelltype equations are used to model a circular cylindrical shell. The static problem of bifurcation of buckled modes from Poisson expansion is analyzed using an iteration scheme and pertubation methods. Analysis shows that although buckling loads are usually simple eigenvalues, they may have arbitrarily large but finite multiplicity when the ratio of the shell's length and circumference is rational. A numerical study of the critical buckling load for simple eigenvalues indicates that the number of waves along the axis of the deformed shell is roughly proportional to the length of the shell, suggesting the possibility of a "characteristic length." Further numerical work indicates that initial postbuckling curves are typically steep, although the load may increase or decrease. It is shown that either a sheet of solutions or two distinct branches bifurcate from a double eigenvalue. Furthermore, a shell may be subject to a uniform torque, even though one is not prescribed at the ends of the shell, through the interaction of two modes with the same number of circumferential waves. Finally, multiple time scale techniques are used to study the dynamic buckling of a rectangular plate as well as a circular cylindrical shell; transition to a new steady state amplitude determined by the nonlinearity is shown. The importance of damping in determining equilibrium configurations independent of initial conditions is illustrated.
Item Type:  Thesis (Dissertation (Ph.D.)) 

Subject Keywords:  (Applied Mathematics) 
Degree Grantor:  California Institute of Technology 
Division:  Physics, Mathematics and Astronomy 
Major Option:  Applied Mathematics 
Thesis Availability:  Public (worldwide access) 
Research Advisor(s): 

Thesis Committee: 

Defense Date:  30 May 1975 
Record Number:  CaltechTHESIS:03292013141424985 
Persistent URL:  https://resolver.caltech.edu/CaltechTHESIS:03292013141424985 
DOI:  10.7907/KYF4PD11 
Default Usage Policy:  No commercial reproduction, distribution, display or performance rights in this work are provided. 
ID Code:  7565 
Collection:  CaltechTHESIS 
Deposited By:  Benjamin Perez 
Deposited On:  29 Mar 2013 21:45 
Last Modified:  05 Aug 2024 21:57 
Thesis Files

PDF
 Final Version
See Usage Policy. 25MB 
Repository Staff Only: item control page