Coupled Analytical Sensitivity Analysis and Optimization of Three-Dimensional Nonlinear Aeroelastic Systems

By Kurt Maute, M. Nikbay, Charbel Farhat. 2001

205 citations recorded by the source corpus.

Subfields: Civil and Structural Engineering, Mechanics of Materials, Statistics and Probability

View Paper: https://www.semanticscholar.org/paper/b72c9aea298ea04f8593078f62770b0d968f6a38

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Civil and Structural Engineering

1. John T. Hwang
2. Joaquim R. Martins
3. M. Allen
4. Juan José Palacios Alonso
5. James Reuther
6. Kurt Maute
7. Richard P. Dwight
8. Ramana V. Grandhi

In Mechanics of Materials

1. Joaquim R. Martins
2. John T. Hwang
3. M. Allen
4. Juan José Palacios Alonso
5. James Reuther
6. Kurt Maute
7. Richard P. Dwight
8. Ramana V. Grandhi

In Statistics and Probability

1. Joaquim R. Martins
2. John T. Hwang
3. Jacques Peter
4. M. Allen
5. Juan José Palacios Alonso
6. James Reuther
7. Kurt Maute
8. Richard P. Dwight

Citations in the corpus

• A coupled-adjoint method for high-fidelity aero-structural optimization (2002, methodology): “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].”
• A Coupled-Adjoint Sensitivity Analysis Method for High-Fidelity Aero-Structural Design (2005, methodology): “However, only recently has the this method been applied to the computation of sensitivities of coupled high-fidelity systems (Martins et al., 2001, 2002; Maute et al., 2001).”
• Adjoint-Based Sensitivity Formulation for Fully Coupled Unsteady Aeroelasticity Problems (2009, background): “The coupling between the fluid and structure equations and the use of sensitivity analysis on such a system has been addressed but primarily from a steady-state standpoint [10,11].”
• Numerical sensitivity analysis for aerodynamic optimization: A survey of approaches (2010, background): “[146], Martins, Alonso and Reuther [147] and Fazzolari [135].”
• Review and Unification of Methods for Computing Derivatives of Multidisciplinary Computational Models (2013, methodology): “Both the coupled direct and adjointmethods have since been applied to the aerostructural design optimization of aircraft wings [12,21,91,92].”
• Conceptual design of aeroelastic structures by topology optimization (2004, methodology): “The algorithm is summarized in Table 1 and described in detail by Maute et al. (2001, 2003) .”