An adaptive machine learning-based optimization method in the aerodynamic analysis of a finite wing under various cruise conditions

Author:

Zhang ZilanORCID,Ao YuORCID,Li ShaofanORCID,Gu Grace X.

Funder

Center for Information Technology Research in the Interest of Society

University of California Berkeley CITRIS and the Banatao Institute

National Science Foundation

Air Force Office of Scientific Research

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Aerospace Engineering,Biomedical Engineering,Civil and Structural Engineering,Environmental Engineering,Computational Mechanics

Reference51 articles.

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2. Aircraft design in the 21st century-implications for design methods;Raj,1998

3. Drag force and drag coefficient;Sadraey,2009

4. Aircraft Design;Kundu,2010

5. Aircraft Design: a Conceptual Approach;Raymer,2012

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