Optimization of aircraft configurations in a multidisciplinary environment
Optimization of aircraft configurations in a multidisciplinary environment
- New search for: Logan, Trent R.
- New search for: Abdi, Frank F.
- New search for: Sobieszczanski-Sobieski, Jaroslaw
- New search for: Logan, Trent R.
- New search for: Abdi, Frank F.
- New search for: Sobieszczanski-Sobieski, Jaroslaw
A decomposition and multidisciplinary optimization methodology for aircraft design is presented, based on multilevel optimization and use of global sensitivity equations to account for interdisciplinary effects. A brief study of a hypersonic cruise vehicle is developed to illustrate methodology. The vehicle is sized for minimum take-off gross weight considering aerodynamics, structures, and mission performance.
Document information
Optimization of aircraft configurations in a multidisciplinary environment
ICAS Congress
1990-01-01
Conference paper
No indication
English
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