A coupled-adjoint method for high-fidelity aero-structural optimization

By Joaquim R. Martins. 2002

89 citations recorded by the source corpus.

View Paper: https://www.semanticscholar.org/paper/8d1de8c1c1ab9d4c6f3a6aca2d527420ace6ca12

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1. James Reuther

Citations in the corpus

• A Coupled-Adjoint Sensitivity Analysis Method for High-Fidelity Aero-Structural Design (2005, methodology): “The foundation for both the coupled analysis procedure and the coupled-adjoint solver is an aero-structural design framework previously developed by the authors (Reuther et al., 1999c; Martins, 2002).”
• The complex-step derivative approximation (2003, unknown): “One of the most complicated examples is a high-fidelity aero-structural solver, which is part of an MDO framework created to solve wing aero-structural design optimization problems [Reuther et al. 1999b; Martins et al. 2002; Martins 2002].”