A computerized system for determining the design layout of an aircraft. The system includes an input module configured to receive a first input data indicating a first value of a first parameter, a first feature database that includes a plurality of feature settings, a feature search module configured to search the first feature database and select a feature setting based on the first value of the first parameter, a central database that includes a plurality of rules governing a design layout of a fuselage, and an optimizing module in communication with the central database and configured to generate an optimal design layout based on the selected feature setting.
DESIGN OPTIMIZER SYSTEM AND METHODS
PROCEDES ET SYSTEMES D'OPTIMISATEUR DE CONCEPTION
2016-09-09
Patent
Elektronische Ressource
Englisch
AIAA | 2022
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