An optimization design method is discussed. This method is based on integrating existing disciplinary analysis and sensitivity analysis techniques by means of generalized sensitivity equations. A generic design system implementing this method is described. The system is being used to design the configuration and internal structure of a supersonic transport wing for optimum performance. This problem combines the disciplines of linear aerodynamics, structures, and performance. Initial results which include the disciplines of aerodynamics and structures in a conventional minimum weight design under static aeroelastic constraints are presented.
Application of Multidisciplinary Optimization Methods to the Design of a Supersonic Transport
1991
7 pages
Report
No indication
English
MULTIDISCIPLINARY DESIGN OPTIMIZATION OF SUPERSONIC TRANSPORT WING USING SURROGATE MODEL
British Library Conference Proceedings | 2010
|British Library Conference Proceedings | 2010
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