Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project

Prajwal Shiva Prakasha; Pier Davide Ciampa; Pierluigi Della Vecchia; Danilo Ciliberti; Mark Voskuij; Dominique Charbonnier; Aidan Jungo; Mengmeng Zhang; Marco Fioriti; Kirill Anisimov; Artur Mirzoyan

doi:10.2514/6.2018-4006

Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project

Prajwal Shiva Prakasha, Pier Davide Ciampa, Pierluigi Della Vecchia, Danilo Ciliberti, Mark Voskuij, Dominique Charbonnier, Aidan Jungo, Mengmeng Zhang, Marco Fioriti, Kirill Anisimov, Artur Mirzoyan

Flight Performance and Propulsion

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

18 Citations (Scopus)

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.

Original language	English
Title of host publication	2018 Aviation Technology, Integration, and Operations Conference
Publisher	American Institute of Aeronautics and Astronautics Inc. (AIAA)
Number of pages	27
ISBN (Electronic)	9781624105562
DOIs	https://doi.org/10.2514/6.2018-4006
Publication status	Published - 2018
Event	18th AIAA Aviation Technology, Integration, and Operations Conference, 2018 - Atlanta, United States Duration: 25 Jun 2018 → 29 Jun 2018

Conference

Conference	18th AIAA Aviation Technology, Integration, and Operations Conference, 2018
Country/Territory	United States
City	Atlanta
Period	25/06/18 → 29/06/18

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10.2514/6.2018-4006

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Prakasha, P. S., Ciampa, P. D., Della Vecchia, P., Ciliberti, D., Voskuij, M., Charbonnier, D., Jungo, A., Zhang, M., Fioriti, M., Anisimov, K., & Mirzoyan, A. (2018). Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project. In 2018 Aviation Technology, Integration, and Operations Conference [AIAA 2018-4006] American Institute of Aeronautics and Astronautics Inc. (AIAA). https://doi.org/10.2514/6.2018-4006

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. / Model based collaborative design & optimization of blended wing body aircraft configuration : AGILE EU project. 2018 Aviation Technology, Integration, and Operations Conference. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2018.

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title = "Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project",

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 {\textquoteleft}AGILE MDAO framework{\textquoteright} 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.",

author = "Prakasha, {Prajwal Shiva} and Ciampa, {Pier Davide} and {Della Vecchia}, Pierluigi and Danilo Ciliberti and Mark Voskuij and Dominique Charbonnier and Aidan Jungo and Mengmeng Zhang and Marco Fioriti and Kirill Anisimov and Artur Mirzoyan",

year = "2018",

doi = "10.2514/6.2018-4006",

language = "English",

booktitle = "2018 Aviation Technology, Integration, and Operations Conference",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

address = "United States",

note = "18th AIAA Aviation Technology, Integration, and Operations Conference, 2018 ; Conference date: 25-06-2018 Through 29-06-2018",

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Prakasha, PS, Ciampa, PD, Della Vecchia, P, Ciliberti, D, Voskuij, M, Charbonnier, D, Jungo, A, Zhang, M, Fioriti, M, Anisimov, K & Mirzoyan, A 2018, Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project. in 2018 Aviation Technology, Integration, and Operations Conference., AIAA 2018-4006, American Institute of Aeronautics and Astronautics Inc. (AIAA), 18th AIAA Aviation Technology, Integration, and Operations Conference, 2018, Atlanta, United States, 25/06/18. https://doi.org/10.2514/6.2018-4006

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 Aviation Technology, Integration, and Operations Conference. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2018. AIAA 2018-4006.

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

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AU - Prakasha, Prajwal Shiva

AU - Ciampa, Pier Davide

AU - Della Vecchia, Pierluigi

AU - Ciliberti, Danilo

AU - Voskuij, Mark

AU - Charbonnier, Dominique

AU - Jungo, Aidan

AU - Zhang, Mengmeng

AU - Fioriti, Marco

AU - Anisimov, Kirill

AU - Mirzoyan, Artur

PY - 2018

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AB - 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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PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)

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ER -

Prakasha PS, Ciampa PD, Della Vecchia P, Ciliberti D, Voskuij M, Charbonnier D et al. Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project. In 2018 Aviation Technology, Integration, and Operations Conference. American Institute of Aeronautics and Astronautics Inc. (AIAA). 2018. AIAA 2018-4006 https://doi.org/10.2514/6.2018-4006

Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project

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