Article
Multi-Fidelity Robust Aerodynamic Design Optimization under Mixed Uncertainty
Proceedings of the 17th AIAA Non-Deterministic Approaches Conference, AIAA SciTech Forum (2015, Kissimmee, FL)
Abstract
The objective of this paper is to present a robust optimization algorithm for computationally efficient airfoil design under mixed (inherent and epistemic) uncertainty using a multi-fidelity approach.
Meeting Name
17th AIAA Non-Deterministic Approaches Conference, AIAA SciTech Forum (2015: Jan. 5-9, Kissimmee, FL)
Department(s)
Mechanical and Aerospace Engineering
Research Center/Lab(s)
Center for High Performance Computing Research
Document Type
Article - Conference proceedings
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2015 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.
Publication Date
1-1-2015
Publication Date
01 Jan 2015
Disciplines
Citation Information
Harsheel R. Shah, Serhat Hosder, Slawomir Koziel, Yonatan Afework Tesfahunegn, et al.. "Multi-Fidelity Robust Aerodynamic Design Optimization under Mixed Uncertainty" Proceedings of the 17th AIAA Non-Deterministic Approaches Conference, AIAA SciTech Forum (2015, Kissimmee, FL) (2015) Available at: http://works.bepress.com/serhat-hosder/22/