Graduation Semester and Year
2005
Language
English
Document Type
Thesis
Degree Name
Master of Science in Mechanical Engineering
Department
Mechanical and Aerospace Engineering
First Advisor
Kent L Lawrence
Abstract
The high computational expense of large non-linear and complex finite element analysis limits or often prohibits the use of conventional codes in engineering design and multidisciplinary optimization. Consequently alternate methods such as Design of experiments (DOE) and Response surface approximation are commonly used to minimize the computational cost of running such analysis and simulation. The basic approach of such methods is to construct a simplified mathematical approximation of the computationally expensive simulation and analysis code, which is then used in place of the original code to facilitate multidisciplinary optimization, design space exploration, reliability analysis etc. When such codes along with powerful finite element analysis tools such as ANSYS are tied with good optimization algorithms, solving complex structural optimization problems are no longer an issue. This research work aims at defining such an automation process in MATLAB that incorporates a response surface approximating tool called MQR which is based on Radial basis function, ANSYS a finite element solver and a suitable gradient based optimization algorithm (SQP). Certain standard test cases are considered that are based on size and dynamic response optimization. The results obtained from the proposed method are compared with ANSYS DesignXplorer goal driven optimization which is based on DOE and also with ANSYS First order optimization technique. The comparison of the results demonstrates the accuracy and effectiveness of the proposed MQR based optimization process.
Disciplines
Aerospace Engineering | Engineering | Mechanical Engineering
License
This work is licensed under a Creative Commons Attribution-NonCommercial-Share Alike 4.0 International License.
Recommended Citation
Menon, Ajaykumar, "Structural Optimization Using ANSYS And Regulated Multiquadric Response Surface Model" (2005). Mechanical and Aerospace Engineering Theses. 590.
https://mavmatrix.uta.edu/mechaerospace_theses/590
Comments
Degree granted by The University of Texas at Arlington