Complete Configuration Aero-Structural Optimization Using a Coupled Sensitivity Analysis Method
By Joaquim R. Martins, Juan José Palacios Alonso, James Reuther. 2002
53 citations recorded by the source corpus.
Subfields: Applied Mathematics, Computational Mechanics, Global and Planetary Change
View Paper: https://www.semanticscholar.org/paper/a3cdb5098c8ee000de861b50c1c0d3d0850d2c42
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In Applied Mathematics
In Computational Mechanics
In Global and Planetary Change
Citations in the corpus
- 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].”
- A coupled-adjoint method for high-fidelity aero-structural optimization (2002, background): “These ideas include multilevel optimization strategies [4, 35], collaborative optimization [12, 37, 17], individual discipline feasible methods [16], as well as integrated coupled optimization procedures [23, 49, 43, 45, 44].”