Simulated Annealing Computational Requirements Reduction for Reliability-Based High-Fidelity Aerodynamic Shape Design

Citation:
Ogot M, Kelly B. "Simulated Annealing Computational Requirements Reduction for Reliability-Based High-Fidelity Aerodynamic Shape Design.". In: 44th AIAA Aerospace Sciences Meeting and Exhibit.; 2006:.

Abstract:

Recent research efforts in Multi-disciplinary Design Optimization (MDO) have concentrated
on the development of optimization methods that incorporate uncertainty present in design
variables and/or from noise variables to perform robust or reliability-based design. This work
presents a simulated annealing (SA) approach within the framework of highfidelity 'black-
box'analysis codes for aerodynamic shape design. The analysis codes are restricted to
inexpensive (seconds per analysis iteration) or moderately expensive (minutes per analysis …

Notes:

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