2018
|
Drougard, Malo Computer-Aided Design for Aircraft Masters Thesis EPFL - CFS Engineering, 2018. Links | BibTeX | Tags: @mastersthesis{ Malo2018_34 ,
title = {Computer-Aided Design for Aircraft},
author = {Malo Drougard},
url = {https://www.agile-project.eu/cloud/index.php/s/5NCYBUiaXmNh3uR},
year = {2018},
date = {2018-09-01},
school = {EPFL - CFS Engineering},
keywords = {},
pubstate = {published},
tppubtype = {mastersthesis}
}
|
Baalbergen, E; Lammen, W; Noskov, N; Ciampa, P D; Moerland, E Integrated collaboration capabilities for competitive aircraft design Conference EASN-CEAS 2018 , Glasgow, UK, 2018. Links | BibTeX | Tags: @conference{ Baalbergen2018_69 ,
title = {Integrated collaboration capabilities for competitive aircraft design},
author = {E. Baalbergen and W. Lammen and N. Noskov and P.D. Ciampa and E. Moerland},
url = {https://www.agile-project.eu/cloud/index.php/s/SoIufBsbYMbGvg8},
year = {2018},
date = {2018-09-01},
address = {Glasgow, UK},
organization = {EASN-CEAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Walther, J N; Gastaldi, A; Jungo, A; Zhang, M; Maierl, R Integration Aspects of the Collaborative Aero-Structural Design of an Unmanned Aerial Vehicle Conference DLRK 2018 , Friedrichshafen, DE, 2018. Links | BibTeX | Tags: @conference{ Walther2018_93 ,
title = {Integration Aspects of the Collaborative Aero-Structural Design of an Unmanned Aerial Vehicle},
author = {J.N. Walther and A. Gastaldi and A. Jungo and M. Zhang and R. Maierl},
url = {https://www.agile-project.eu/cloud/index.php/s/1LLvkJlcrxcazSF},
year = {2018},
date = {2018-09-01},
address = {Friedrichshafen, DE},
organization = {DLRK 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Ciampa, P D; Nagel, B Streamlining Cross-Organizational Aircraft Development Processes: an Overview of the AGILE Project Conference ICAS 2018 , Belo Horizonte, Brazil, 2018. BibTeX | Tags: @conference{ Ciampa2018_98 ,
title = {Streamlining Cross-Organizational Aircraft Development Processes: an Overview of the AGILE Project},
author = {P.D. Ciampa and B. Nagel},
year = {2018},
date = {2018-09-01},
address = {Belo Horizonte, Brazil},
organization = {ICAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Prakasha, P S; Ciampa, P D; Della Vecchia, P; Ciliberti, D; Voskuijl, M; Charbonnier, D; Jungo, A; Fioriti, M; Anisimov, K; Mirzoyan, A Multidisciplinary Design Analysis of Blended Wing Body through Collaborative Design Approach: AGILE EU Project Conference ICAS 2018 , Belo Horizonte, Brazil, 2018. BibTeX | Tags: @conference{ Prakasha2018_110 ,
title = {Multidisciplinary Design Analysis of Blended Wing Body through Collaborative Design Approach: AGILE EU Project},
author = {P.S. Prakasha and P.D. Ciampa and P. {Della Vecchia} and D. Ciliberti and M. Voskuijl and D. Charbonnier and A. Jungo and M. Fioriti and K. Anisimov and A. Mirzoyan},
year = {2018},
date = {2018-09-01},
address = {Belo Horizonte, Brazil},
organization = {ICAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Maierl, R; Gastaldi, A; Daoud, F; Walther, J N; Ciampa, P D; Jungo, A; Zhang, M Aero-Structural Optimization of a Male Configuration in the AGILE MDO Framework Conference ICAS 2018 , Belo Horizonte, Brazil, 2018. Links | BibTeX | Tags: @conference{ Maierl2018_79 ,
title = {Aero-Structural Optimization of a Male Configuration in the AGILE MDO Framework},
author = {R. Maierl and A. Gastaldi and F. Daoud and J.N. Walther and P.D. Ciampa and A. Jungo and M. Zhang},
url = {https://www.agile-project.eu/cloud/index.php/s/p55SINI9eJBJYoP},
year = {2018},
date = {2018-09-01},
address = {Belo Horizonte, Brazil},
organization = {ICAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Torrigiani, F; Bussemaker, J; Ciampa, P D; Fioriti, M; Tomasella, F; Aigner, B; Rajpal, D; Timmermans, H; Savelyev, A; Charbonnier, D Design of the Strut Braced Wing aircraft in the AGILE Collaborative MDO Framework Conference ICAS 2018 , Belo Horizonte, Brazil, 2018. Links | BibTeX | Tags: @conference{ Torrigiani2018_81 ,
title = {Design of the Strut Braced Wing aircraft in the AGILE Collaborative MDO Framework},
author = {F. Torrigiani and J. Bussemaker and P.D. Ciampa and M. Fioriti and F. Tomasella and B. Aigner and D. Rajpal and H. Timmermans and A. Savelyev and D. Charbonnier},
url = {https://www.agile-project.eu/cloud/index.php/s/AYfmOZCBYHqRqHj},
year = {2018},
date = {2018-09-01},
address = {Belo Horizonte, Brazil},
organization = {ICAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Stingo, L; Della Vecchia, P; Cerino, G MDO Applications to Conventional and Novel Turboprop Aircraft within the AGILE European Project Conference ICAS 2018 , Belo Horizonte, Brazil, 2018. Links | BibTeX | Tags: @conference{ Stingo2018_95 ,
title = {MDO Applications to Conventional and Novel Turboprop Aircraft within the AGILE European Project},
author = {L. Stingo and P. {Della Vecchia} and G. Cerino},
url = {https://www.agile-project.eu/cloud/index.php/s/AKvrf44eu1upZMA},
year = {2018},
date = {2018-09-01},
address = {Belo Horizonte, Brazil},
organization = {ICAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Rajpal, D; De Breuker, R; Timmermans, H; Lammen, W; Torrigiani, F Including Aeroelastic Tailoring in the Conceptual Design Process of a Strut Braced Wing Conference ICAS 2018 , Belo Horizonte, Brazil, 2018. Links | BibTeX | Tags: @conference{ Rajpal2018_87 ,
title = {Including Aeroelastic Tailoring in the Conceptual Design Process of a Strut Braced Wing},
author = {D. Rajpal and R. {De Breuker} and H. Timmermans and W. Lammen and F. Torrigiani},
url = {https://www.agile-project.eu/cloud/index.php/s/4l3rB8oUX6a3Fb0},
year = {2018},
date = {2018-09-01},
address = {Belo Horizonte, Brazil},
organization = {ICAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Della Vecchia, P; Aigner, B; van Gent, I; Ciampa, P D; Prakasha, P S Collaborative Open Source Aircraft Design Framework for Education – AGILE Academy Initiatives and Results Conference ICAS 2018 , Belo Horizonte, Brazil, 2018. BibTeX | Tags: @conference{ Della2018_105 ,
title = {Collaborative Open Source Aircraft Design Framework for Education – AGILE Academy Initiatives and Results},
author = {P. {Della Vecchia} and B. Aigner and I. {van Gent} and P.D. Ciampa and P.S. Prakasha},
year = {2018},
date = {2018-09-01},
address = {Belo Horizonte, Brazil},
organization = {ICAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Spieck, M; Aigner, B; Prakasha, P S; Ciampa, P D MDO as a Socio-Technical System – a small Contribution to Collaborative engineering Conference ICAS 2018 , Belo Horizonte, Brazil, 2018. Links | BibTeX | Tags: @conference{ Spieck2018_83 ,
title = {MDO as a Socio-Technical System – a small Contribution to Collaborative engineering},
author = {M. Spieck and B. Aigner and P.S. Prakasha and P.D. Ciampa},
url = {https://www.agile-project.eu/cloud/index.php/s/ItEqdXKYPpEsznD},
year = {2018},
date = {2018-09-01},
address = {Belo Horizonte, Brazil},
organization = {ICAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Mirzoyan, A; Isyanov, A; Fokin, D; D’Ippolito, R; Lombardi, R Multiobjective Multiparametric Optimization of Propulsion System for Advanced Civil Aircraft in Distributed Environment of Collaborative MDO System developed in AGILE project Conference ICAS 2018 , Belo Horizonte, Brazil, 2018. Links | BibTeX | Tags: @conference{ Mirzoyan2018_174 ,
title = {Multiobjective Multiparametric Optimization of Propulsion System for Advanced Civil Aircraft in Distributed Environment of Collaborative MDO System developed in AGILE project},
author = {A. Mirzoyan and A. Isyanov and D. Fokin and R. D’Ippolito and R. Lombardi},
url = {https://www.agile-project.eu/cloud/index.php/s/EbMrZbdXM0U6HqS},
year = {2018},
date = {2018-09-01},
address = {Belo Horizonte, Brazil},
organization = {ICAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Fioriti, M; Boggero, L; Mirzoyan, A; Isyanov, A Studies on Propulsion and on-board systems mathing in AGILE Project Distributed Collaborative MDO Environment applying for Advanced Regional and Medium Hauljet Conference ICAS 2018 , Belo Horizonte, Brazil, 2018. Links | BibTeX | Tags: @conference{ Fioriti2018_159 ,
title = {Studies on Propulsion and on-board systems mathing in AGILE Project Distributed Collaborative MDO Environment applying for Advanced Regional and Medium Hauljet},
author = {M. Fioriti and L. Boggero and A. Mirzoyan and A. Isyanov},
url = {https://www.agile-project.eu/cloud/index.php/s/fNzmUJmmOx6qK8p},
year = {2018},
date = {2018-09-01},
address = {Belo Horizonte, Brazil},
organization = {ICAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Anisimov, K; Savelyev, A; Kursakov, I; Lysenkov, A; Mirzoyan, A; Prakasha, P S Propulsion System – Airframe Integration and Optimization of Civil Aircraft – AGILE EU Project Conference ICAS 2018 , Belo Horizonte, Brazil, 2018. Links | BibTeX | Tags: @conference{ Anisimov2018_94 ,
title = {Propulsion System – Airframe Integration and Optimization of Civil Aircraft – AGILE EU Project},
author = {K. Anisimov and A. Savelyev and I. Kursakov and A. Lysenkov and A. Mirzoyan and P.S. Prakasha},
url = {https://www.agile-project.eu/cloud/index.php/s/ANIjkFyULacgbvT},
year = {2018},
date = {2018-09-01},
address = {Belo Horizonte, Brazil},
organization = {ICAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Boggero, L; Fioriti, M; Tomasella, F; Ciampa, P D Integration of on-board systems preliminary design discipline within a Collaborative 3rd Generation MDO Framework Conference ICAS 2018 , Belo Horizonte, Brazil, 2018. Links | BibTeX | Tags: @conference{ Boggero2018_113 ,
title = {Integration of on-board systems preliminary design discipline within a Collaborative 3rd Generation MDO Framework},
author = {L. Boggero and M. Fioriti and F. Tomasella and P.D. Ciampa},
url = {https://www.agile-project.eu/cloud/index.php/s/ndwneygNVyWgLVg},
year = {2018},
date = {2018-09-01},
address = {Belo Horizonte, Brazil},
organization = {ICAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Toktaliev, P Communication between PS and Aircraft Systems in collective MDO SYSTEM in AGILE Project Conference ICAS 2018 , Belo Horizonte, Brazil, 2018. BibTeX | Tags: @conference{ Toktaliev2018_87 ,
title = {Communication between PS and Aircraft Systems in collective MDO SYSTEM in AGILE Project},
author = {P. Toktaliev},
year = {2018},
date = {2018-09-01},
address = {Belo Horizonte, Brazil},
organization = {ICAS 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Boggero, Luca Design Techniques to Support Aircraft Systems Development in a Collaborative Environment PhD Thesis Politecnico di Torino, 2018. Links | BibTeX | Tags: @phdthesis{ Luca2018_88 ,
title = {Design Techniques to Support Aircraft Systems Development in a Collaborative Environment},
author = {Luca Boggero},
url = {https://www.agile-project.eu/cloud/index.php/s/46YXUPIhQpIscZH},
year = {2018},
date = {2018-07-01},
school = {Politecnico di Torino},
keywords = {},
pubstate = {published},
tppubtype = {phdthesis}
}
|
Ciampa, P D; Nagel, B AGILE the Next Generation of Collaborative MDO: Achievements and Open Challenges Conference paper 2018-3249 , AIAA Aviation 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ Ciampa2018_80 ,
title = {AGILE the Next Generation of Collaborative MDO: Achievements and Open Challenges},
author = {P.D. Ciampa and B. Nagel},
url = {https://www.agile-project.eu/cloud/index.php/s/fU2nGxCv1tMp0Dk},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-3249},
address = {Atlanta, US},
organization = {AIAA Aviation 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Bartoli, N; Lefebvre, T; Dubreuil, S; Panzeri, M; d’Ippolito, R; Anisimov, K; Savelyev, A Robust Nacelle Optimization Design investigated in the AGILE European Project Conference paper 2018-3250 , AIAA Aviation 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ Bartoli2018_77 ,
title = {Robust Nacelle Optimization Design investigated in the AGILE European Project},
author = {N. Bartoli and T. Lefebvre and S. Dubreuil and M. Panzeri and R. d’Ippolito and K. Anisimov and A. Savelyev},
url = {https://www.agile-project.eu/cloud/index.php/s/fhRLOyLrAM8Z3Mc},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-3250},
address = {Atlanta, US},
organization = {AIAA Aviation 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Lefebvre, T; Bartoli, N; Dubreuil, S; Panzeri, M; Lombardi, R; Lammen, W; Zhang, M; van Gent, I; Ciampa, P D A clustered and surrogate-based MDA use case for MDO scenarios in AGILE project, AGILE the Next Generation of Collaborative MDO: Achievements and Open Challenges Conference paper 2018-3252 , AIAA Aviation 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ Lefebvre2018_161 ,
title = {A clustered and surrogate-based MDA use case for MDO scenarios in AGILE project, AGILE the Next Generation of Collaborative MDO: Achievements and Open Challenges},
author = {T. Lefebvre and N. Bartoli and S. Dubreuil and M. Panzeri and R. Lombardi and W. Lammen and M. Zhang and I. {van Gent} and P.D. Ciampa},
url = {https://www.agile-project.eu/cloud/index.php/s/bI5GzbAajNbWeIR},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-3252},
address = {Atlanta, US},
organization = {AIAA Aviation 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
de Wit, A J; Lammen, W; Timmermans, H; Vankan, J; Charbonnier, D; van der Laan, T; Ciampa, P D A collaborative design method for the aircraft supply chain multi-level optimization Conference paper 2018-3253 , AIAA Aviation 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ de2018_84 ,
title = {A collaborative design method for the aircraft supply chain multi-level optimization},
author = {A.J. {de Wit} and W. Lammen and H. Timmermans and J. Vankan and D. Charbonnier and T. {van der Laan} and P.D. Ciampa},
url = {https://www.agile-project.eu/cloud/index.php/s/zNUdeiZD5pA1ofC},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-3253},
address = {Atlanta, US},
organization = {AIAA Aviation 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
van Gent, I; Aigner, B; Beijer, B; La Rocca, G A Critical Look at Design Automation Solutions for Collaborative MDO in the AGILE Paradigm Conference paper 2018-3251 , AIAA Aviation 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ van2018_90 ,
title = {A Critical Look at Design Automation Solutions for Collaborative MDO in the AGILE Paradigm},
author = {I. {van Gent} and B. Aigner and B. Beijer and G. {La Rocca}},
url = {https://www.agile-project.eu/cloud/index.php/s/jt4sKfVAiAs1aB3},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-3251},
address = {Atlanta, US},
organization = {AIAA Aviation 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Della Vecchia, P; Ciampa, P D; Prakasha, P S; Aigner, B; van Gent, I MDO Framework for university research collaboration: AGILE Academy initiative and Outcomes Conference paper 2018-3254 , AIAA Aviation 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ Della2018_90 ,
title = {MDO Framework for university research collaboration: AGILE Academy initiative and Outcomes},
author = {P. {Della Vecchia} and P.D. Ciampa and P.S. Prakasha and B. Aigner and I. {van Gent}},
url = {https://www.agile-project.eu/cloud/index.php/s/5yifjK3kXFdbx1c},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-3254},
address = {Atlanta, US},
organization = {AIAA Aviation 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Dubreuil, S; Bartoli, N; Lefebvre, T; Cogu, C Efficient global multidisciplinary optimisation based on surrogate models Conference paper 2018-3745 , AIAA Aviation 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ Dubreuil2018_73 ,
title = {Efficient global multidisciplinary optimisation based on surrogate models},
author = {S. Dubreuil and N. Bartoli and T. Lefebvre and C. Cogu},
url = {https://www.agile-project.eu/cloud/index.php/s/YR3SEDsbxOLburi},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-3745},
address = {Atlanta, US},
organization = {AIAA Aviation 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
van der Laan, T; Hootsmans, L Consequences of Multi or Single disciplinary optimization results on aircraft component cost and weight Conference paper 2018-3026 , AIAA Aviation 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ van2018_103 ,
title = {Consequences of Multi or Single disciplinary optimization results on aircraft component cost and weight},
author = {T. {van der Laan} and L. Hootsmans},
url = {https://www.agile-project.eu/cloud/index.php/s/zW8JxHsJzWDC9EV},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-3026},
address = {Atlanta, US},
organization = {AIAA Aviation 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Della Vecchia, P; Stingo, L; Nicolosi, F; Cerino, G; Ciampa, P D; Prakasha, P S; Fioriti, M; Zhang, M; Mirzoyan, A; Aigner, B; Charbonnier, D Advanced Turboprop Multidisciplinary optimization within AGILE project Conference paper 2018-3205 , AIAA Aviation 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ Della2018_70 ,
title = {Advanced Turboprop Multidisciplinary optimization within AGILE project},
author = {P. {Della Vecchia} and L. Stingo and F. Nicolosi and G. Cerino and P.D. Ciampa and P.S. Prakasha and M. Fioriti and M. Zhang and A. Mirzoyan and B. Aigner and D. Charbonnier},
url = {https://www.agile-project.eu/cloud/index.php/s/SnVNvLJRPr699T4},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-3205},
address = {Atlanta, US},
organization = {AIAA Aviation 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Torrigiani, F; Ciampa, P D Aerostructural Optimization with Unsteady Aero-elastic Constraints in a Collaborative MDO Environment Conference paper 2018-3879 , AIAA Aviation 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ Torrigiani2018_101 ,
title = {Aerostructural Optimization with Unsteady Aero-elastic Constraints in a Collaborative MDO Environment},
author = {F. Torrigiani and P.D. Ciampa},
url = {https://www.agile-project.eu/cloud/index.php/s/sJZXXrOjkjEdQwB},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-3879},
address = {Atlanta, US},
organization = {AIAA Aviation 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Fioriti, M; Boggero, L; Tomasella, F; Mirzoyan, A; Isyanov, A; Prakasha, P S Propulsion and on-board system integration for regional, me Conference paper 2018-2847 , AIAA Propulsion & Energy 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ Fioriti2018_59 ,
title = {Propulsion and on-board system integration for regional, me},
author = {M. Fioriti and L. Boggero and F. Tomasella and A. Mirzoyan and A. Isyanov and P.S. Prakasha},
url = {https://www.agile-project.eu/cloud/index.php/s/lqZ1n3Kky9SGkMt},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-2847},
address = {Atlanta, US},
organization = {AIAA Propulsion & Energy 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Mirzoyan, A; Fioriti, M; Boggero, L; Tomasella, F Preliminary Study on OBS Electrification Efficiency for Advanced Supersonic Business and Medium Jet with Unified Engines, AIAA Propulsion & Energy Conference paper 2018-2851 , AIAA Propulsion & Energy 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ Mirzoyan2018_146 ,
title = {Preliminary Study on OBS Electrification Efficiency for Advanced Supersonic Business and Medium Jet with Unified Engines, AIAA Propulsion & Energy},
author = {A. Mirzoyan and M. Fioriti and L. Boggero and F. Tomasella},
url = {https://www.agile-project.eu/cloud/index.php/s/a0FhiFljD3zYzB8},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-2851},
address = {Atlanta, US},
organization = {AIAA Propulsion & Energy 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Mirzoyan, A; Isyanov, A; Fioriti, M; Boggero, L; Tomasella, F; Prakasha, P S; Ciampa, P D Propulsion System for BWB configurations in the AGILE project Conference paper 2018-2848 , AIAA Propulsion & Energy 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ Mirzoyan2018_61 ,
title = {Propulsion System for BWB configurations in the AGILE project},
author = {A. Mirzoyan and A. Isyanov and M. Fioriti and L. Boggero and F. Tomasella and P.S. Prakasha and P.D. Ciampa},
url = {https://www.agile-project.eu/cloud/index.php/s/244uENb7y9grCoY},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-2848},
address = {Atlanta, US},
organization = {AIAA Propulsion & Energy 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Mirzoyan, A; Isyanov, A; Cerino, G; Della Vecchia, P; Stingo, L; Fioriti, M; Boggero, L; Tomasella, F; Prakasha, P S Comparative study of advanced turboprop aircraft with wing and rear mounted propulsion system in the AGILE EU project Conference paper 2018-2849 , AIAA Propulsion & Energy 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ Mirzoyan2018_117 ,
title = {Comparative study of advanced turboprop aircraft with wing and rear mounted propulsion system in the AGILE EU project},
author = {A. Mirzoyan and A. Isyanov and G. Cerino and P. {Della Vecchia} and L. Stingo and M. Fioriti and L. Boggero and F. Tomasella and P.S. Prakasha},
url = {https://www.agile-project.eu/cloud/index.php/s/EWfhX1LBf6cKsbT},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-2849},
address = {Atlanta, US},
organization = {AIAA Propulsion & Energy 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Mirzoyan, A; Isyanov, A; Toktaliev, P; Froidmont, A; Lombardi, R; D’Ippolito, R Development of the Engine Meta-Models for Advanced Regional JET MDO in the Scope of Agile Project Conference paper 2018-4850 , AIAA Propulsion & Energy 2018 , Atlanta, US, 2018. Links | BibTeX | Tags: @conference{ Mirzoyan2018_97 ,
title = {Development of the Engine Meta-Models for Advanced Regional JET MDO in the Scope of Agile Project},
author = {A. Mirzoyan and A. Isyanov and P. Toktaliev and A. Froidmont and R. Lombardi and R. D’Ippolito},
url = {https://www.agile-project.eu/cloud/index.php/s/7iwdguVvTX9j8Tp},
year = {2018},
date = {2018-06-01},
volume = {paper 2018-4850},
address = {Atlanta, US},
organization = {AIAA Propulsion & Energy 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Ciampa, P D Conference ILA Berlin 2018 , Berlin, Germany, 2018. BibTeX | Tags: @conference{ Ciampa2018_0 ,
author = {P.D. Ciampa},
year = {2018},
date = {2018-04-01},
address = {Berlin, Germany},
organization = {ILA Berlin 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Ferrari, Flavia Impact of different subsystems architectures on aircraft engines in terms of Specific Fuel Consumption Masters Thesis Politecnico di Torino, 2018. Links | BibTeX | Tags: @mastersthesis{ Flavia2018_102 ,
title = {Impact of different subsystems architectures on aircraft engines in terms of Specific Fuel Consumption},
author = {Flavia Ferrari},
url = {https://www.agile-project.eu/cloud/index.php/s/0lHVi4Nj12OR00T},
year = {2018},
date = {2018-03-01},
school = {Politecnico di Torino},
keywords = {},
pubstate = {published},
tppubtype = {mastersthesis}
}
|
Dubreuil, S; Bartoli, N; Gogu, C; Lefebvre, T Multidisciplinary Optimization based on surrogate models Conference International Workshop on Optimization and Learning (OLA) , Alicante, Spain, 2018. Links | BibTeX | Tags: @conference{ Dubreuil2018_56 ,
title = {Multidisciplinary Optimization based on surrogate models},
author = {S. Dubreuil and N. Bartoli and C. Gogu and T. Lefebvre},
url = {https://www.agile-project.eu/cloud/index.php/s/Dldfmf1tlEhJSro},
year = {2018},
date = {2018-02-01},
address = {Alicante, Spain},
organization = {International Workshop on Optimization and Learning (OLA) ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Grazioli, Pasquale An automatic CAD-Maker for high-fidelity analysis within AGILE European project Masters Thesis University of Naples « Federico II », 2018. BibTeX | Tags: @mastersthesis{ Pasquale2018_78 ,
title = {An automatic CAD-Maker for high-fidelity analysis within AGILE European project},
author = {Pasquale Grazioli},
year = {2018},
date = {2018-01-01},
school = {University of Naples « Federico II »},
keywords = {},
pubstate = {published},
tppubtype = {mastersthesis}
}
|
Jungo, A; Zhang, M; Vos, J B; Rizzi, A Benchmarking New CEASIOM with CPACS Adoption for Aerodynamic Analysis and Flight Simulation Journal Article Aircraft Engineering and Aerospace Technology, 90 (4), 2018. Links | BibTeX | Tags: @article{ Jungo2018_91 ,
title = {Benchmarking New CEASIOM with CPACS Adoption for Aerodynamic Analysis and Flight Simulation},
author = {A. Jungo and M. Zhang and J.B. Vos and A. Rizzi},
url = {https://www.emeraldinsight.com/doi/full/10.1108/AEAT-11-2016-0204},
year = {2018},
date = {2018-01-01},
journal = {Aircraft Engineering and Aerospace Technology},
volume = {90},
number = {4},
publisher = {Emeraldinsight},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
|
Dubreuil, S; Bartoli, N; Gogu, C; Lefebvre, T; Mas Colomer, J Extreme value oriented random field discretization based on an hybrid polynomial chaos expansion — Kriging approach Journal Article Computer Methods in Applied Mechanics and Engineering, 332 , 2018. Abstract | Links | BibTeX | Tags: @article{ Dubreuil2018_115 ,
title = {Extreme value oriented random field discretization based on an hybrid polynomial chaos expansion — Kriging approach},
author = {S. Dubreuil and N. Bartoli and C. Gogu and T. Lefebvre and J. {Mas Colomer}},
url = {https://www.agile-project.eu/cloud/index.php/s/Cs1AhsyewEFmBlp},
year = {2018},
date = {2018-01-01},
journal = {Computer Methods in Applied Mechanics and Engineering},
volume = {332},
abstract = {This article addresses the characterization of extreme value statistics of continuous second order random field. More precisely, it focuses on the parametric study of engineering models under uncertainty. Hence, the quantity of interest of this model is defined on both a parametric space and a stochastic space. Moreover, we consider that the model is computationally expensive to evaluate. For this reason it is assumed that uncertainty propagation, at a single point of the parametric space, is achieved by polynomial chaos expansion. The main contribution of the present study is the development of an adaptive approach for the discretization of the random field modeling the quantity of interest. Objective of this new approach is to focus the computational budget over the areas of the parametric space where the minimum or the maximum of the field is likely to be for any realization of the stochastic parameters. To this purpose two original random field representations, based on polynomial chaos expansion and Kriging interpolation, are introduced. Moreover, an original adaptive enrichment scheme based on Kriging is proposed. Advantages of this approach with respect to accuracy and computational cost are demonstrated on several numerical examples. The proposed method is also illustrated on the parametric study of an aircraft wing under uncertainty.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
This article addresses the characterization of extreme value statistics of continuous second order random field. More precisely, it focuses on the parametric study of engineering models under uncertainty. Hence, the quantity of interest of this model is defined on both a parametric space and a stochastic space. Moreover, we consider that the model is computationally expensive to evaluate. For this reason it is assumed that uncertainty propagation, at a single point of the parametric space, is achieved by polynomial chaos expansion. The main contribution of the present study is the development of an adaptive approach for the discretization of the random field modeling the quantity of interest. Objective of this new approach is to focus the computational budget over the areas of the parametric space where the minimum or the maximum of the field is likely to be for any realization of the stochastic parameters. To this purpose two original random field representations, based on polynomial chaos expansion and Kriging interpolation, are introduced. Moreover, an original adaptive enrichment scheme based on Kriging is proposed. Advantages of this approach with respect to accuracy and computational cost are demonstrated on several numerical examples. The proposed method is also illustrated on the parametric study of an aircraft wing under uncertainty. |
Fioriti, M; Boggero, L; Corpino, S; Prakasha, P S; Ciampa, P D; Nagel, B The Effect of Sub-systems Design Parameters on Preliminary Aircraft Design in a Multidisciplinary Design Environment Journal Article Transportation Research Procedia, 29 , 2018. Abstract | Links | BibTeX | Tags: @article{ Fioriti2018_116 ,
title = {The Effect of Sub-systems Design Parameters on Preliminary Aircraft Design in a Multidisciplinary Design Environment},
author = {M. Fioriti and L. Boggero and S. Corpino and P.S. Prakasha and P.D. Ciampa and B. Nagel},
url = {https://www.agile-project.eu/cloud/index.php/s/Znioz7OITLJE4b0},
year = {2018},
date = {2018-01-01},
journal = {Transportation Research Procedia},
volume = {29},
abstract = {The remarkable complexity of the aircraft design is due to several reasons and one of these is certainly the high number of completely different design disciplines involved in the process. Many efforts are spent to harmonize and optimize the aircraft design trying to consider all disciplines together with the same level of detail. Within the ongoing H2020 AGILE research, an aircraft MDO (Multidisciplinary Design Optimization) process is setting up linking several design tools and, above all, competences together. This paper focuses on the evaluation of the effects of the main on -board systems design parameters on the other disciplines. Starting from a baseline aircraft (AGILE DC1 regional turbofan), the effect of each parameters have been quantified in terms of variation of aircraft weight, fuel consumption and engine performance. This analysis represents a useful starting point to better understand the importance and the influence of novel On-Board Systems configurations, such as More and All Electric, to the overall aircraft design.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
The remarkable complexity of the aircraft design is due to several reasons and one of these is certainly the high number of completely different design disciplines involved in the process. Many efforts are spent to harmonize and optimize the aircraft design trying to consider all disciplines together with the same level of detail. Within the ongoing H2020 AGILE research, an aircraft MDO (Multidisciplinary Design Optimization) process is setting up linking several design tools and, above all, competences together. This paper focuses on the evaluation of the effects of the main on -board systems design parameters on the other disciplines. Starting from a baseline aircraft (AGILE DC1 regional turbofan), the effect of each parameters have been quantified in terms of variation of aircraft weight, fuel consumption and engine performance. This analysis represents a useful starting point to better understand the importance and the influence of novel On-Board Systems configurations, such as More and All Electric, to the overall aircraft design. |
Zhang, M; Jungo, A; Gastaldi, A; Melin, T Aircraft Geometry and Meshing with Common Language Schema CPACS for Variable-Fidelity MDO Applications Journal Article Aerospace, 5 (2), 2018. Abstract | Links | BibTeX | Tags: @article{ Zhang2018_102 ,
title = {Aircraft Geometry and Meshing with Common Language Schema CPACS for Variable-Fidelity MDO Applications},
author = {M. Zhang and A. Jungo and A. Gastaldi and T. Melin},
url = {https://www.agile-project.eu/cloud/index.php/s/3jK4uQ9m3acKMbp},
year = {2018},
date = {2018-01-01},
journal = {Aerospace},
volume = {5},
number = {2},
abstract = {Abstract: This paper discusses multi-fidelity aircraft geometry modeling and meshing with the common language schema CPACS. The CPACS interfaces are described, and examples of variable fidelity aerodynamic analysis results applied to the reference aircraft are presented. Finally, we discuss three control surface deflection models for Euler computation.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
Abstract: This paper discusses multi-fidelity aircraft geometry modeling and meshing with the common language schema CPACS. The CPACS interfaces are described, and examples of variable fidelity aerodynamic analysis results applied to the reference aircraft are presented. Finally, we discuss three control surface deflection models for Euler computation. |
van Gent, I; La Rocca, G; Hoogreef, M F M CMDOWS: a proposed new standard to store and exchange MDO systems Journal Article CEAS Aeronautical Journal, 2018. Links | BibTeX | Tags: @article{ van2018_65 ,
title = {CMDOWS: a proposed new standard to store and exchange MDO systems},
author = {I. {van Gent} and G. {La Rocca} and M.F.M. Hoogreef},
url = {https://www.agile-project.eu/cloud/index.php/s/LveDnZlgqHPBy2P},
year = {2018},
date = {2018-01-01},
journal = {CEAS Aeronautical Journal},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
|
Aigner, B; van Gent, I; La Rocca, G; Stumpf, E; Veldhuis, L Graph-Based Algorithms and Data Driven Documents for Formulation and Visualization of Large MDO Systems Journal Article CEAS Aeronautical Journal, 2018. Links | BibTeX | Tags: @article{ Aigner2018_103 ,
title = {Graph-Based Algorithms and Data Driven Documents for Formulation and Visualization of Large MDO Systems},
author = {B. Aigner and I. {van Gent} and G. {La Rocca} and E. Stumpf and L. Veldhuis},
url = {https://www.agile-project.eu/cloud/index.php/s/GPMa6UUIHPA1WXz},
year = {2018},
date = {2018-01-01},
journal = {CEAS Aeronautical Journal},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
|
2017
|
Kodali Rao, Nithin Influence of Parametric Modelling of Wing Subsystems on the Aircraft Design and Performance Masters Thesis TU Delft, 2017. Links | BibTeX | Tags: @mastersthesis{ Kodali2017_91 ,
title = {Influence of Parametric Modelling of Wing Subsystems on the Aircraft Design and Performance},
author = {Nithin {Kodali Rao}},
url = {https://www.agile-project.eu/cloud/index.php/s/3eOlYMgrFvO7F0t},
year = {2017},
date = {2017-12-01},
school = {TU Delft},
keywords = {},
pubstate = {published},
tppubtype = {mastersthesis}
}
|
Smeets, Thais Development of a Knowledge Based Engineering Application to Support Conceptual Fuselage Design Masters Thesis TU Delft, 2017. Links | BibTeX | Tags: @mastersthesis{ Smeets2017_94 ,
title = {Development of a Knowledge Based Engineering Application to Support Conceptual Fuselage Design},
author = {Thais Smeets},
url = {https://www.agile-project.eu/cloud/index.php/s/AOH5S6lgQvVFg35#},
year = {2017},
date = {2017-12-01},
school = {TU Delft},
keywords = {},
pubstate = {published},
tppubtype = {mastersthesis}
}
|
Nollman, Maximilian Development of a Hybrid Electric Powertrain for Large Commercial Transport Aircraft Masters Thesis RWTH Aachen, 2017. Links | BibTeX | Tags: @mastersthesis{ Nollman2017_83 ,
title = {Development of a Hybrid Electric Powertrain for Large Commercial Transport Aircraft},
author = {Maximilian Nollman},
url = {https://www.agile-project.eu/cloud/index.php/s/gI83KKH20ywAaeL},
year = {2017},
date = {2017-12-01},
school = {RWTH Aachen},
keywords = {},
pubstate = {published},
tppubtype = {mastersthesis}
}
|
De Vries, Daniel Towards the Industrialization of MDAO Masters Thesis TU Delft, 2017. Links | BibTeX | Tags: @mastersthesis{ De2017_37 ,
title = {Towards the Industrialization of MDAO},
author = {Daniel {De Vries}},
url = {https://www.agile-project.eu/cloud/index.php/s/lKzcnAuyf9NlY5l},
year = {2017},
date = {2017-12-01},
school = {TU Delft},
keywords = {},
pubstate = {published},
tppubtype = {mastersthesis}
}
|
Aigner, B; van Gent, I; La Rocca, G; Stumpf, E Using graph-based algorithms and data-driven documents for formulation and visualization of large MDO systems. Conference Paper 173 , 6th CEAS Air & Space Conference Aerospace Europe , Bucharest, Romania, 2017. Abstract | Links | BibTeX | Tags: @conference{ Aigner2017_110 ,
title = {Using graph-based algorithms and data-driven documents for formulation and visualization of large MDO systems.},
author = {B. Aigner and I. {van Gent} and G. {La Rocca} and E. Stumpf},
url = {https://www.agile-project.eu/cloud/index.php/s/mbdufb7vnnMRb3Y},
year = {2017},
date = {2017-10-01},
volume = {Paper 173},
address = {Bucharest, Romania},
organization = {6th CEAS Air & Space Conference Aerospace Europe ,},
abstract = {A new system is presented that enables the visualization of large multidisciplinary design optimization (MDO) problems and their solution strategy. This visualization system is the result of a cooperation between RWTH Aachen University and Delft University of Technology (DUT) within the EU project AGILE. In AGILE, col- laborative MDO is performed in large, heterogeneous teams of experts by solving MDO problems using a collection of design and analysis tools. The two main phases of such a collaborative MDO project are the formulation and the execution phase. This paper focuses on the visualizations required to support the for- mulation phase of the MDO problem. In this phase three main steps have been identified: the set-up of the repository of interconnected tools, the definition of the MDO problem at hand, and the determination of the solution strategy to solve that MDO problem. KADMOS, an open-source MDO support system developed by DUT, uses graph-based analysis to formulate an MDO problem and its solution strategy, based on the disciplinary analyses available in a repository. The results of KADMOS are stored in a standardized format called CMDOWS, which is eventually used to trigger the execution phase by means of a simulation workflow platform of choice. Although based on XML, the readability of the CMDOWS file is quite poor also for MDO experts, especially for large MDO systems involving thousands of variables, thus preventing visual inspection of the formalized MDO problem. Providing visualization capabilities to thoroughly inspect the outcome of the three aforementioned formulation steps becomes a key factor to enable the specification of large MDO sys- tems in a heterogeneous team. Therefore, one of the main hurdles for using MDO as a development process can be removed. Conventional visualization methods (such as N2-charts, functional dependency tables, and design structure matrices) have major scalability limitations. Therefore VISTOMS, a dynamic visualization package based on the open-source visualization library D3.js, was developed by RWTH Aachen to enable the visualization and inspection of the different MDO system specification steps. The developed visualization capabilities are demonstrated by means of a wing design optimization problem performed at DUT. As shown in this use case, VISTOMS enables the visualization and inspection of a large MDO system containing more than ten different aircraft design tools, interlinking thousands of variables.},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
A new system is presented that enables the visualization of large multidisciplinary design optimization (MDO) problems and their solution strategy. This visualization system is the result of a cooperation between RWTH Aachen University and Delft University of Technology (DUT) within the EU project AGILE. In AGILE, col- laborative MDO is performed in large, heterogeneous teams of experts by solving MDO problems using a collection of design and analysis tools. The two main phases of such a collaborative MDO project are the formulation and the execution phase. This paper focuses on the visualizations required to support the for- mulation phase of the MDO problem. In this phase three main steps have been identified: the set-up of the repository of interconnected tools, the definition of the MDO problem at hand, and the determination of the solution strategy to solve that MDO problem. KADMOS, an open-source MDO support system developed by DUT, uses graph-based analysis to formulate an MDO problem and its solution strategy, based on the disciplinary analyses available in a repository. The results of KADMOS are stored in a standardized format called CMDOWS, which is eventually used to trigger the execution phase by means of a simulation workflow platform of choice. Although based on XML, the readability of the CMDOWS file is quite poor also for MDO experts, especially for large MDO systems involving thousands of variables, thus preventing visual inspection of the formalized MDO problem. Providing visualization capabilities to thoroughly inspect the outcome of the three aforementioned formulation steps becomes a key factor to enable the specification of large MDO sys- tems in a heterogeneous team. Therefore, one of the main hurdles for using MDO as a development process can be removed. Conventional visualization methods (such as N2-charts, functional dependency tables, and design structure matrices) have major scalability limitations. Therefore VISTOMS, a dynamic visualization package based on the open-source visualization library D3.js, was developed by RWTH Aachen to enable the visualization and inspection of the different MDO system specification steps. The developed visualization capabilities are demonstrated by means of a wing design optimization problem performed at DUT. As shown in this use case, VISTOMS enables the visualization and inspection of a large MDO system containing more than ten different aircraft design tools, interlinking thousands of variables. |
Fioriti, M; Boggero, L; Corpino, S; Prakasha, P S; Ciampa, P D; Nagel, B The Effect of Sub-systems Design Parameters on Preliminary Aircraft Design in a Multidisciplinary Design Environment. Conference Paper 245 , 6th CEAS Air & Space Conference Aerospace Europe , Bucharest, Romania, 2017. Abstract | Links | BibTeX | Tags: @conference{ Fioriti2017_117 ,
title = {The Effect of Sub-systems Design Parameters on Preliminary Aircraft Design in a Multidisciplinary Design Environment.},
author = {M. Fioriti and L. Boggero and S. Corpino and P.S. Prakasha and P.D. Ciampa and B. Nagel},
url = {https://www.agile-project.eu/cloud/index.php/s/K2mdxSzqDxMOG90},
year = {2017},
date = {2017-10-01},
volume = {Paper 245},
address = {Bucharest, Romania},
organization = {6th CEAS Air & Space Conference Aerospace Europe ,},
abstract = {The remarkable complexity of the aircraft design is due to several reasons and one of these is certainly the high number of completely different design disciplines involved in the process. Many efforts are spent to harmonize and optimize the aircraft design trying to consider all disciplines together with the same level of detail. Within the ongoing H2020 AGILE research, an aircraft MDO (Multidisciplinar y Design Optimization) process is setting up linking several design tools and, above all, competences together. This paper focuses on the evaluation of the effects of the main on-board systems design parameters on the other disciplines. Starting from a baseline aircraft (A GILE DC1 regional turbofan), the effect of each parameters have been quantified in terms of variation of aircraft weight, fuel consumption and engine performance. This analysis represents a useful starting point to better understand the importance and the influence of novel On-Board Systems configurations, such as More and All Electric, to the overall aircraft design.},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
The remarkable complexity of the aircraft design is due to several reasons and one of these is certainly the high number of completely different design disciplines involved in the process. Many efforts are spent to harmonize and optimize the aircraft design trying to consider all disciplines together with the same level of detail. Within the ongoing H2020 AGILE research, an aircraft MDO (Multidisciplinar y Design Optimization) process is setting up linking several design tools and, above all, competences together. This paper focuses on the evaluation of the effects of the main on-board systems design parameters on the other disciplines. Starting from a baseline aircraft (A GILE DC1 regional turbofan), the effect of each parameters have been quantified in terms of variation of aircraft weight, fuel consumption and engine performance. This analysis represents a useful starting point to better understand the importance and the influence of novel On-Board Systems configurations, such as More and All Electric, to the overall aircraft design. |
Della Vecchia, P; Nicolosi, F; Ruocco, M; Stingo, L; De Marco, A An improved method for transport aircraft for high lift aerodynamic prediction. Conference Paper 254 , 6th CEAS Air & Space Conference Aerospace Europe , Bucharest, Romania, 2017. Abstract | Links | BibTeX | Tags: @conference{ Della2017_79 ,
title = {An improved method for transport aircraft for high lift aerodynamic prediction.},
author = {P. {Della Vecchia} and F. Nicolosi and M. Ruocco and L. Stingo and A. {De Marco}},
url = {https://www.agile-project.eu/cloud/index.php/s/PY5Vg0lo8hBT4jn},
year = {2017},
date = {2017-10-01},
volume = {Paper 254},
address = {Bucharest, Romania},
organization = {6th CEAS Air & Space Conference Aerospace Europe ,},
abstract = {The aim of this work is the development of a methodology to predict lift characteristics for transport aircraft in the whole flight envelope, useful in the preliminary aircraft design stage. The purpose is an attempt to improve the classical methodologies for wing load distribution and lift prediction, considering the airfoils aerodynamic characteristics until stall and post stall conditions during the process, and modifying 2D characteristics in case of high lift devices to take into account 3D effects introduced by the devices themselves. The method is a modification of Nasa Blackwell procedure, capable to predict wing stall aerodynamic characteristics for both clean and flapped configuration. As far the high lift devices effect is concerned, the improved method works substituting clean airfoil aerodynamic characteristics with the flapped aerodynamics ones, and introducing a correction to evaluate the 3D effects induced by high lift devices geometrical discontinuities. The results of the developed method have been compared with CFD and experimental data showing good agreement, making available a fast and reliable method, useful in preliminary aircraft design.},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
The aim of this work is the development of a methodology to predict lift characteristics for transport aircraft in the whole flight envelope, useful in the preliminary aircraft design stage. The purpose is an attempt to improve the classical methodologies for wing load distribution and lift prediction, considering the airfoils aerodynamic characteristics until stall and post stall conditions during the process, and modifying 2D characteristics in case of high lift devices to take into account 3D effects introduced by the devices themselves. The method is a modification of Nasa Blackwell procedure, capable to predict wing stall aerodynamic characteristics for both clean and flapped configuration. As far the high lift devices effect is concerned, the improved method works substituting clean airfoil aerodynamic characteristics with the flapped aerodynamics ones, and introducing a correction to evaluate the 3D effects induced by high lift devices geometrical discontinuities. The results of the developed method have been compared with CFD and experimental data showing good agreement, making available a fast and reliable method, useful in preliminary aircraft design. |
Lombardi, R; Fioriti, M; Boggero, L; Lo Verde, L; Catino, N; Mirzoyan, A; D’Ippolito, R Automated Selection of Airliner Optimal On-board Systems Architecture within MDO Collaborative Environment. Conference Paper 258 , 6th CEAS Air & Space Conference Aerospace Europe , Bucharest, Romania, 2017. Abstract | Links | BibTeX | Tags: @conference{ Lombardi2017_107 ,
title = {Automated Selection of Airliner Optimal On-board Systems Architecture within MDO Collaborative Environment.},
author = {R. Lombardi and M. Fioriti and L. Boggero and L. {Lo Verde} and N. Catino and A. Mirzoyan and R. D’Ippolito},
url = {https://www.agile-project.eu/cloud/index.php/s/YVrwhDUTDZ2PEJY},
year = {2017},
date = {2017-10-01},
volume = {Paper 258},
address = {Bucharest, Romania},
organization = {6th CEAS Air & Space Conference Aerospace Europe ,},
abstract = {The test case described in the paper is a multidisciplinary design optimization (MDO) aimed at the identification of the best on-board system architecture on the basis of its production and operative costs. Other researcher have focused their attention in the selection of more suitable system architecture [1], however, in the present work, one of the key objective was to develop a collaborative multidisciplinary optimization environment able to propagate the effects of the chosen architecture on engine and actuator fairings and consequently on engine performance (fuel consumption) and aerodynamic properties (total drag). The collaborative MDO has been implemented using a commercial PIDO, Optimus by Noesis Solutions; this has been used to connect four different analysis tools (developed and operated by Politecnico di Torino, Leonardo Aircraft-Alenia and CIAM) adopting the communication protocols that have been developed within AGILE.},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
The test case described in the paper is a multidisciplinary design optimization (MDO) aimed at the identification of the best on-board system architecture on the basis of its production and operative costs. Other researcher have focused their attention in the selection of more suitable system architecture [1], however, in the present work, one of the key objective was to develop a collaborative multidisciplinary optimization environment able to propagate the effects of the chosen architecture on engine and actuator fairings and consequently on engine performance (fuel consumption) and aerodynamic properties (total drag). The collaborative MDO has been implemented using a commercial PIDO, Optimus by Noesis Solutions; this has been used to connect four different analysis tools (developed and operated by Politecnico di Torino, Leonardo Aircraft-Alenia and CIAM) adopting the communication protocols that have been developed within AGILE. |
