Font Size: a A A

Airfoil shape optimization using variable-complexity methods

Posted on:2006-11-12Degree:M.A.ScType:Thesis
University:University of Toronto (Canada)Candidate:Thokala, PraveenFull Text:PDF
GTID:2452390008960148Subject:Engineering
Abstract/Summary:
This thesis deals with variable-complexity optimization, which consists of either using high- and low-fidelity models of the analysis or using variable parameterization of the optimization problem to reduce the computational cost of the optimization process. In this thesis, we present a variable-fidelity framework that is mathematically robust. We then present the results on analytical test cases for the framework and variable-parameterization method, which involves using different design variables during the course of the optimization process. The framework and the variable-parameterization method are then used to perform airfoil shape optimization. The variable-fidelity framework performed satisfactorily for most cases while a thorough mathematical study is needed for the variable-parameterization method.
Keywords/Search Tags:Optimization, Method, Variable-fidelity framework
Related items