Multifidelity Data Fusion: Application to Blended-Wing-Body Multidisciplinary Analysis Under Uncertainty
Author:
Affiliation:
1. Aurora Flight Sciences, Cambridge, Massachusetts 02142
2. The Boeing Company, Huntington Beach, California 92647
3. University of Texas at Austin, Austin, Texas 78712
Funder
Boeing
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference40 articles.
1. Design of the Blended Wing Body Subsonic Transport
2. Control allocation challenges and requirements for the Blended Wing Body
3. Multicontrol Surface Optimization for Blended Wing–Body Under Handling Quality Constraints
4. Alternative Trim Analysis Formulations for Vehicles with Redundant Multi-Axis Control Surfaces
5. Multi-fidelity optimization via surrogate modelling
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