A Multisubstructure-Based Method for the Assessment of Displacement and Stress in a Fluid–Structure Interaction Framework
Author:
Affiliation:
1. School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China
2. Flying College, Beihang University, Beijing 100191, China
3. China Research and Development Academy of Machinery Equipment, Beijing 100089, China
Abstract
Funder
Frontier Cross-Fund Project of Beihang Univeristy
Publisher
MDPI AG
Link
https://www.mdpi.com/2226-4310/11/6/423/pdf
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3. Taylor, R. (2006, January 3–8). The role of optimization in component structural design: Application to the F-35 joint strike fighter. Proceedings of the 25th International Congress of the Aeronautical Sciences, Hamburg, Germany.
4. Recent progress, challenges and outlook for multidisciplinary structural optimization of aircraft and aerial vehicles;Corrado;Prog. Aerosp. Sci.,2022
5. Integrated structure/control/aerodynamic synthesis of actively controlled composite wings;Livne;J. Aircr.,1993
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