Efficient Monolithic Solution Algorithm for High-Fidelity Aerostructural Analysis and Optimization
Author:
Affiliation:
1. University of Toronto, Toronto, Ontario M3H 5T6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056163
Reference52 articles.
1. A coupled aero-structural optimization method for complete aircraft configurations
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4. High-Fidelity Aerostructural Design Optimization of a Supersonic Business Jet
5. A Coupled-Adjoint Sensitivity Analysis Method for High-Fidelity Aero-Structural Design
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