Advanced turboprop multidisciplinary design and optimization within AGILE project
2018
The present paper deals with the design, analysis and optimization of a 90 passengers turboprop aircraft with a design range of 1200 nautical miles and a cruise Mach number equal to 0.56. The pres
cribed aircraft is one of the use cases of the AGILE European project, aiming to provide a 3rd generation of multidisciplinary design and optimization chain, following the collaborative and remote aircraft design paradigm, through an heterogenous team of experts.
The multidisciplinary aircraft design analysis is set-up involving tools provided by AGILE partners distributed worldwide and run locally from partners side. A complete design of
experiment, focused on wing planform variables, is performed to build
response surfaces
suitable for optimization purposes. The goal of the optimization is the direct operati
ng
cost
,
subject to wing design variables and top
-
level aircraft requirements.
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