Title

Multi-Fidelity Robust Aerodynamic Design Optimization under Mixed Uncertainty

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.


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