Multi-Fidelity Robust Aerodynamic Design Optimization under Mixed Uncertainty

Author

Harsheel R. Shah
Serhat Hosder, Missouri University of Science and TechnologyFollow
Slawomir Koziel
Yonatan Afework Tesfahunegn
Leifur Leifsson

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.

Recommended Citation

H. R. Shah 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), American Institute of Aeronautics and Astronautics (AIAA), Jan 2015.

The definitive version is available at https://doi.org/10.2514/6.2015-0917

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

01 Jan 2015