Model based collaborative design &amp; optimization of blended wing body aircraft configuration

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Model based collaborative design & optimization of blended wing body aircraft configuration

AGILE EU project

Conference Paper (2018)

Author(s)

Prajwal Shiva Prakasha (Deutsches Zentrum für Luft- und Raumfahrt (DLR))

Pier Davide Ciampa (Deutsches Zentrum für Luft- und Raumfahrt (DLR))

Pierluigi Della Vecchia (Università degli Studi di Napoli Federico II)

Danilo Ciliberti (Università degli Studi di Napoli Federico II)

Mark Voskuij (TU Delft - Aerospace Engineering)

Dominique Charbonnier (CFSE)

Aidan Jungo (CFSE)

Mengmeng Zhang (AIRINNOVA AB)

Marco Fioriti (Politecnico di Torino)

Kirill Anisimov (Central Aerohydrodynamic Institute (TsAGI))

Artur Mirzoyan (CIAM)

Research Group

Flight Performance and Propulsion

DOI related publication

https://doi.org/10.2514/6.2018-4006 Final published version

To reference this document use

https://resolver.tudelft.nl/uuid:afdc88bf-73d2-4c71-986e-441690a277b2

More Info

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Publication Year

2018

Language

English

Research Group

Flight Performance and Propulsion

Article number

AIAA 2018-4006

ISBN (electronic)

9781624105562

Event

18th AIAA Aviation Technology, Integration, and Operations Conference, 2018 (2018-06-25 - 2018-06-29), Atlanta, United States

Downloads counter

335

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.