Date of Award
Spring 2001
Document Type
Dissertation
Degree Name
Doctor of Philosophy (PhD)
Department
Mechanical & Aerospace Engineering
Program/Concentration
Mechanical Engineering
Committee Director
Gene Hou
Committee Member
Chuh Mei
Committee Member
Sebastian Bawab
Committee Member
Stephen Cupschalk
Abstract
It is quite common in the industry to use various interface methods, such as welding, fasteners, bolts, adhesive bonding, etc., to join substructures together. The quality of the assembled structure is directly related to the type of the interface methods used in the manufacturing process. Thus, it is important to include the interface conditions as part of design variables in any design process. To this end, this work develops a reanalysis method that can efficiently analyze structures with variations on the interface conditions. This reanalysis method is based upon a new two-step substructuring technique. The first step performs substructural level analyses for each of the isolated substructures. Any commercially rated structural analysis code is allowed to be used in this step. The results of the first step are then used to form a reduced order matrix equation in terms of the interface reactions. Once the interface reactions are calculated, the displacements and stresses in each of the substructure can be conveniently calculated. In this proposed method, only the reduced order matrix equation in Step 2 is required to be resolved for structures with different interface conditions.
The first pail of the work will discuss the derivation and implementation aspects of the substructuring technique. Later, the technique is used to support a simple genetic algorithm for placement design optimization of spot welds. Assessment of the proposed method via numerical study is summarized at the end of the dissertation.
Rights
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DOI
10.25777/pg1y-8r19
ISBN
9780493178233
Recommended Citation
Wang, Yang.
"A Substructuring Technique With Application to Spot Weld Placement Design"
(2001). Doctor of Philosophy (PhD), Dissertation, Mechanical & Aerospace Engineering, Old Dominion University, DOI: 10.25777/pg1y-8r19
https://digitalcommons.odu.edu/mae_etds/288