Archivio Istituzionale della RicercaNovel configuration design choices may help achieve revolutionary goals for reducing fuel burn, emission and noise, set by Flightpath 2050. One such advance configuration is a blended wing body. Due to multi-diciplinary nature of the configuration, several partners with disciplinary expertise collaborate in a Model driven ‘AGILE MDAO framework’ to design and evaluate the novel configuration. The objective of this research are: • To create and test a model based collaborative framework using AGILE Paradigm for novel configuration design & optimization, involving large multinational team. Reduce setup time for complex MDO problem. • Through Multi fidelity design space exploration, evaluate aerodynamic performance • The BWB disciplinary analysis models such as aerodynamics, propulsion, onboard systems, S&C were integrated and intermediate results are published in this report.
Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project / Prakasha, Prajwal Shiva; Ciampa, Pier Davide; Della Vecchia, Pierluigi; Ciliberti, Danilo; Voskuij, Mark; Charbonnier, Dominique; Jungo, Aidan; Zhang, Mengmeng; Fioriti, Marco; Anisimov, Kirill; Mirzoyan, Artur. - ELETTRONICO. - (2018). (Intervento presentato al convegno 18th AIAA Aviation Technology, Integration, and Operations Conference, 2018 tenutosi a usa nel 2018) [10.2514/6.2018-4006].
Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project
Fioriti, Marco;
2018
Abstract
Novel configuration design choices may help achieve revolutionary goals for reducing fuel burn, emission and noise, set by Flightpath 2050. One such advance configuration is a blended wing body. Due to multi-diciplinary nature of the configuration, several partners with disciplinary expertise collaborate in a Model driven ‘AGILE MDAO framework’ to design and evaluate the novel configuration. The objective of this research are: • To create and test a model based collaborative framework using AGILE Paradigm for novel configuration design & optimization, involving large multinational team. Reduce setup time for complex MDO problem. • Through Multi fidelity design space exploration, evaluate aerodynamic performance • The BWB disciplinary analysis models such as aerodynamics, propulsion, onboard systems, S&C were integrated and intermediate results are published in this report.
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https://hdl.handle.net/11583/2729892
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