In this paper, we discuss the use of a sensitivity equation method to compute,t-ri vat i ves for optimization based design algorithms. The problem of designing an optimal fore!bod y simulator is used to motivate the algorithm and to illustrate the basic ideas. Finally. wke indicate how an existing CFD code can be modified to compute sensitivities and a nmnwrical example is presented. By....... D{ _ b!tK-J'')
We report on development and validation of a discrete sensitivity solver for the BAE SYSTEMS/Airbus...
Fundamental equations of aerodynamic sensitivity analysis and approximate analysis for the two dimen...
The computational cost associated with the use of high-fidelity Computational Fluid Dynamics (CFD) m...
The effects of sensitivity analysis on the performance of aerodynamic design were evaluated. Sensiti...
No specific solutions are offered, nor verified by applications, for its subject problem which is se...
A new and efficient procedure for aerodynamic shape optimization is presented. The salient lineament...
© 1998 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.The effec...
The Sensitivity-Equation approach is implemented to determine sensitivity derivatives in the framewo...
The effects of sensitivities on the performance of aerodynamic design optimization were evaluated. S...
The effects of sensitivity derivatives on the performance of aerodynamic design optimization were ev...
grantor: University of TorontoThe flow sensitivity approach for aerodynamic optimization ...
© 1996 by the American Institute of Aeronautics and Astronautics, Inc. All rights resewed.The paper ...
A study was performed to evaluate the effects of different flow solvers, optimization methods, and d...
Accurate computation of sensitivity derivatives is becoming an important item in Computational Fluid...
AbstractA discrete semianalytical sensitivity analysis procedure has been developed for calculating ...
We report on development and validation of a discrete sensitivity solver for the BAE SYSTEMS/Airbus...
Fundamental equations of aerodynamic sensitivity analysis and approximate analysis for the two dimen...
The computational cost associated with the use of high-fidelity Computational Fluid Dynamics (CFD) m...
The effects of sensitivity analysis on the performance of aerodynamic design were evaluated. Sensiti...
No specific solutions are offered, nor verified by applications, for its subject problem which is se...
A new and efficient procedure for aerodynamic shape optimization is presented. The salient lineament...
© 1998 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.The effec...
The Sensitivity-Equation approach is implemented to determine sensitivity derivatives in the framewo...
The effects of sensitivities on the performance of aerodynamic design optimization were evaluated. S...
The effects of sensitivity derivatives on the performance of aerodynamic design optimization were ev...
grantor: University of TorontoThe flow sensitivity approach for aerodynamic optimization ...
© 1996 by the American Institute of Aeronautics and Astronautics, Inc. All rights resewed.The paper ...
A study was performed to evaluate the effects of different flow solvers, optimization methods, and d...
Accurate computation of sensitivity derivatives is becoming an important item in Computational Fluid...
AbstractA discrete semianalytical sensitivity analysis procedure has been developed for calculating ...
We report on development and validation of a discrete sensitivity solver for the BAE SYSTEMS/Airbus...
Fundamental equations of aerodynamic sensitivity analysis and approximate analysis for the two dimen...
The computational cost associated with the use of high-fidelity Computational Fluid Dynamics (CFD) m...