Multifidelity optimization under uncertainty for a tailless aircraft

This paper presents a multifidelity method for optimization under uncertainty for aerospace problems. In this work, the effectiveness of the method is demonstrated for the robust optimization of a tailless aircraft that is based on the Boeing Insitu ScanEagle. Aircraft design is often affected by un...

Full description

Bibliographic Details
Main Authors: Jasa, John, Martins, Joaquim R. R. A., Chaudhuri, Anirban, Willcox, Karen E
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Format: Article
Published: American Institute of Aeronautics and Astronautics 2018
Online Access:http://hdl.handle.net/1721.1/115165
https://orcid.org/0000-0002-2281-3067
https://orcid.org/0000-0003-2156-9338