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 - Flight Performance and Propulsion)

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
More Info
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Publication Year
2018
Language
English
Research Group
Flight Performance and Propulsion
ISBN (electronic)
9781624105562

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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