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.

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. - (2018), pp. 1-27. (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

Della Vecchia, Pierluigi
Writing – Review & Editing
;
Ciliberti, Danilo
Writing – Review & Editing
;
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.
2018
9781624105562
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. - (2018), pp. 1-27. (Intervento presentato al convegno 18th AIAA Aviation Technology, Integration, and Operations Conference, 2018 tenutosi a usa nel 2018) [10.2514/6.2018-4006].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11588/736404
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