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Overall Aircraft Design: From the open-source FAST-OAD to its training branch

Journal of physics. Conference series, 2023-06, Vol.2526 (1), p.12029

2023

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Tightly coupled aeroelastic model implementation dedicated to fast aeroelastic tailoring optimisation of high aspect ratio composite wing

Journal of fluids and structures, 2020-04, Vol.94, p.102930, Article 102930

2020

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Performance Improvement of Small Unmanned Aerial Vehicles Through Gust Energy Harvesting

Journal of aircraft, 2018-03, Vol.55 (2), p.741-754

2018

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Multidisciplinary Design Optimization Framework with Coupled Derivative Computation for Hybrid Aircraft

Journal of aircraft, 2020-07, Vol.57 (4), p.715-729

2020

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Automated sizing chain of aircraft structures: A Vertical Tail Plane use case

Journal of physics. Conference series, 2023-06, Vol.2526 (1), p.12031

2023

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Optimization of a hydrogen-based hybrid propulsion system under aircraft performance constraints

Chinese journal of aeronautics, 2023-05, Vol.36 (5), p.41-56

2023

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Modeling and Design Optimization of an Electric Environmental Control System for Commercial Passenger Aircraft

Aerospace, 2023-03, Vol.10 (3), p.260

2023

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Wing Structural Model for Overall Aircraft Design of Distributed Electric Propulsion General Aviation and Regional Aircraft

Aerospace, 2022-01, Vol.9 (1), p.5

2022

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Challenges with using primer IDs to improve accuracy of next generation sequencing

PloS one, 2015-03, Vol.10 (3), p.e0119123-e0119123

2015

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Performance improvement of small-scale rotors by passive blade twist control

Journal of fluids and structures, 2015-05, Vol.55, p.25-41

2015

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Bioinspired wind field estimation—part 1: Angle of attack measurements through surface pressure distribution

International journal of micro air vehicles, 2018-09, Vol.10 (3), p.273-284

2018

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Enhancing preliminary aircraft design through operational considerations: a data-driven approach

IOP conference series. Materials Science and Engineering, 2021-01, Vol.1024 (1), p.12057

2021

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Preliminary Sizing of a Medium Range Blended Wing-Body using a Multidisciplinary Design Analysis Approach

MATEC Web of Conferences, 2018-01, Vol.233, p.14-9

2018

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Parametric model of aircraft external geometry as a component of FAST-OAD aircraft preliminary design system

Journal of physics. Conference series, 2023-06, Vol.2526 (1), p.12030

2023

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Performance Enhancement of Tilt-Body Micro Air Vehicle by Use of Orthotropic Laminated Proprotors

Applied Mechanics and Materials, 2016-01, Vol.819, p.585-590

2016

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Benchmark of different aerodynamic solvers on wing aero-propulsive interactions

IOP conference series. Materials Science and Engineering, 2022-02, Vol.1226 (1), p.12008

2022

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Sensitivity Analysis and Optimization of a Liquid Cooling Thermal Management System for Hybrid Fuel Cell Aircraft

Journal of physics. Conference series, 2024-03, Vol.2716 (1), p.12011

2024

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From FAST to FAST-OAD: An open source framework for rapid Overall Aircraft Design

IOP conference series. Materials Science and Engineering, 2021-01, Vol.1024 (1), p.12062

2021

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An Application of Adaptive Blades on Convertible MAVs

International journal of micro air vehicles, 2013-12, Vol.5 (4), p.229-243

2013

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Spectral project - application of FAST-OAD code to the conceptual design of a hydrogen fuelled commercial aircraft

IOP conference series. Materials Science and Engineering, 2022-02, Vol.1226 (1), p.12027

2022

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Aerodynamic model of propeller–wing interaction for distributed propeller aircraft concept

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2020-08, Vol.234 (10), p.1688-1705

2020

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A hybrid approach of machine learning and expert knowledge for projection of aircraft operability

IOP conference series. Materials Science and Engineering, 2022-02, Vol.1226 (1), p.12046

2022

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Integrated static and dynamic modeling of an ionic polymer–metal composite actuator

Journal of intelligent material systems and structures, 2015-07, Vol.26 (10), p.1164-1178

2015

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Genome evolution by transformation, expansion and contraction (GETEC)

BioSystems, 2015-09, Vol.135, p.15-34

2015

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A generalization of substitution evolution models of nucleotides to genetic motifs

Journal of theoretical biology, 2011-11, Vol.288, p.73-83

2011

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Overall Aircraft Design: From the open-source FAST-OAD to its training branch

Tightly coupled aeroelastic model implementation dedicated to fast aeroelastic tailoring optimisation of high aspect ratio composite wing

Performance Improvement of Small Unmanned Aerial Vehicles Through Gust Energy Harvesting

Multidisciplinary Design Optimization Framework with Coupled Derivative Computation for Hybrid Aircraft

Automated sizing chain of aircraft structures: A Vertical Tail Plane use case

Optimization of a hydrogen-based hybrid propulsion system under aircraft performance constraints

Modeling and Design Optimization of an Electric Environmental Control System for Commercial Passenger Aircraft

Wing Structural Model for Overall Aircraft Design of Distributed Electric Propulsion General Aviation and Regional Aircraft

Challenges with using primer IDs to improve accuracy of next generation sequencing

Performance improvement of small-scale rotors by passive blade twist control

Bioinspired wind field estimation—part 1: Angle of attack measurements through surface pressure distribution

Enhancing preliminary aircraft design through operational considerations: a data-driven approach

Preliminary Sizing of a Medium Range Blended Wing-Body using a Multidisciplinary Design Analysis Approach

Parametric model of aircraft external geometry as a component of FAST-OAD aircraft preliminary design system

Performance Enhancement of Tilt-Body Micro Air Vehicle by Use of Orthotropic Laminated Proprotors

Benchmark of different aerodynamic solvers on wing aero-propulsive interactions

Sensitivity Analysis and Optimization of a Liquid Cooling Thermal Management System for Hybrid Fuel Cell Aircraft

From FAST to FAST-OAD: An open source framework for rapid Overall Aircraft Design

An Application of Adaptive Blades on Convertible MAVs

Spectral project - application of FAST-OAD code to the conceptual design of a hydrogen fuelled commercial aircraft

Aerodynamic model of propeller–wing interaction for distributed propeller aircraft concept

A hybrid approach of machine learning and expert knowledge for projection of aircraft operability

Integrated static and dynamic modeling of an ionic polymer–metal composite actuator

Genome evolution by transformation, expansion and contraction (GETEC)

A generalization of substitution evolution models of nucleotides to genetic motifs

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