Date of Award
Summer 1996
Document Type
Thesis
Degree Name
Master of Science (MS)
Department
Mechanical & Aerospace Engineering
Program/Concentration
Mechanical Engineering
Committee Director
Gene Jean-Win Hou
Committee Member
Jen K. Huang
Committee Member
Yozo Mikata
Call Number for Print
Special Collections; LD4331.E56 T39
Abstract
Design optimization provides an organized, systematic, and efficient method for obtaining design improvements based upon a specified measure of design performance. In the multidisciplinary design optimization (MDO) environment efficient optimization techniques allow complex designs to be improved by managing conflicting disciplinary design goals so as to improve the global design. This thesis studies the implementation issues surrounding MDO techniques and strategies. To facilitate this investigation two testbed problems have been selected for study. These problems consider two approaches to the conceptual design of an aeroelastic wing. The first approach is based on an idealized, two-dimensional representation of an airfoil under the action of an aerodynamic load. The second approach considers a three-dimensional finite element plate model coupled with a Computational Fluid Dynamics (CFD) aerodynamic model based on linear full potential flow equations.
Three MDO strategies were evaluated in this thesis: a loosely-coupled (sequential) disciplinary approach; a tightly-coupled multidisciplinary approach and an uncoupled (parallel) approach that provide coupling via a separate coordination scheme based on prescribed coupling parameters. A code was created that included modules for aerodynamic and structural analysis, sensitivity analysis and optimization. Structural optimization results are provided by the research software, ADS and are based on an efficient sensitivity analysis methodology built upon the ADIFOR symbolic processor system. A separate chapter is provided to discuss sensitivity analysis.
Recent trends have been toward monolithic engineering analysis codes that require huge computational resources often on the order of a supercomputer. For MDO a coupling between large scale disciplinary codes means that available computer resources cannot be taken for granted. This thesis considers the opportunities for coarse-grained parallelization in the MDO environment using the new task-parallel Fortran preprocessor, Fortran-M.
Results show that the coarse-grained parallel implementation is effective for specific MDO strategies where the analysis and optimization operations of individual disciplines can proceed concurrently. Results from the application of the various MDO strategies show very similar values for loosely-coupled (disciplinary) and the tightly coupled (multidisciplinary) optimums for the thesis problem. The sensitivity analysis implementation for this thesis was found to be efficient and robust. Further, sensitivity results demonstrated the utility of the discrete adjoint formulation for MDO.
Rights
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DOI
10.25777/07xp-kg79
Recommended Citation
Taylor, Rodney A..
"A Study of the Numerical Implementation of Multidisciplinary Design Optimization Strategies"
(1996). Master of Science (MS), Thesis, Mechanical & Aerospace Engineering, Old Dominion University, DOI: 10.25777/07xp-kg79
https://digitalcommons.odu.edu/mae_etds/721
Included in
Aerodynamics and Fluid Mechanics Commons, Fluid Dynamics Commons, Numerical Analysis and Computation Commons