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Faculté des Sciences appliquées
Faculté des Sciences appliquées
MASTER THESIS

Master thesis and internship[BR]- Master's thesis : Development of a preliminary aircraft design optimization framework[BR]- Integration internship

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Van Den Berghe, Jérome ULiège
Promotor(s) : Terrapon, Vincent ULiège
Date of defense : 30-Jun-2025/1-Jul-2025 • Permalink : http://hdl.handle.net/2268.2/23387
Details
Title : Master thesis and internship[BR]- Master's thesis : Development of a preliminary aircraft design optimization framework[BR]- Integration internship
Translated title : [en] Development of a preliminary aircraft design optimization framework
Author : Van Den Berghe, Jérome ULiège
Date of defense  : 30-Jun-2025/1-Jul-2025
Advisor(s) : Terrapon, Vincent ULiège
Committee's member(s) : Dechamps, Paul ULiège
Andrianne, Thomas ULiège
Crovato, Adrien 
Language : English
Number of pages : 106
Keywords : [en] Aircraft design
[en] Raptor
[en] Multidisciplinary optimization
Discipline(s) : Engineering, computing & technology > Aerospace & aeronautics engineering
Target public : Researchers
Professionals of domain
Student
Institution(s) : Université de Liège, Liège, Belgique
Degree: Master en ingénieur civil en aérospatiale, à finalité spécialisée en "aerospace engineering"
Faculty: Master thesis of the Faculté des Sciences appliquées

Abstract

[en] Traditional aircraft design methods rely on iterative procedures with limited automation and weak
couplingbetweendisciplines, resultinginatime-consumingprocessthatcanleadtosuboptimaldesigns.
Multidisciplinary Design Optimization (MDO) emerges as a powerful alternative to overcome these
limitations.
This thesis presents the development of RAPTOR (Rapid Aircraft Preliminary Optimization and
Refinement), a modular, open-source framework tailored for early-stage aircraft design. RAPTOR
addresses the shortcomings of conventional approaches by integrating a fully multidisciplinary opti
mization architecture built on top of OpenMDAO, enabling efficient coordination between geometry,
aerodynamics, structures, propulsion, stability, weight estimation, and performance evaluation. The
frameworksupportsrapidconfigurationandrefinementofbothconventionalandunconventionalaircraft
through gradient-based optimization and multi-fidelity analyses.
Validation is carried out through benchmark studies and optimization cases, including a tailless
unmanned aerial vehicle (UAV) and a single-seat aerobatic aircraft, illustrating the ability of RAPTOR
to handle diverse aircraft configurations.


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Author

  • Van Den Berghe, Jérome ULiège Université de Liège > Master ing. civ. aéro., fin. spéc. aer. eng.

Promotor(s)

Committee's member(s)

  • Dechamps, Paul ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Modélisation et contrôle des écoulements turbulents
    ORBi View his publications on ORBi
  • Andrianne, Thomas ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Aéroélasticité et Aérodynamique expérimentale
    ORBi View his publications on ORBi
  • Crovato, Adrien








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