2018
|
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 @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}
}
|
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 @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 @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}
}
|
Drougard, Malo Computer-Aided Design for Aircraft Masters Thesis EPFL - CFS Engineering, 2018. Links | BibTeX @mastersthesis{ Drougard2018_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}
}
|
Vos, J B; Charbonnier, D; Siikonen, T; Salminen, E; Gehri, A; Stephani, P Swiss/Finnish Collaboration on Aero-elastic Simulations for the F/A-18 Fighter Conference AIAA-2018-3642 , AIAA Aviation 2018 , Atlanta, 2018. Links | BibTeX @conference{ Vos2018_78 ,
title = {Swiss/Finnish Collaboration on Aero-elastic Simulations for the F/A-18 Fighter},
author = {J.B. Vos and D. Charbonnier and T. Siikonen and E. Salminen and A. Gehri and P. Stephani},
url = {https://cfse.ch/wp-content/uploads/2019/05/AIAA-2018-3642.pdf},
year = {2018},
date = {2018-06-01},
volume = {AIAA-2018-3642},
address = {Atlanta},
organization = {AIAA Aviation 2018 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
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 @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},
doi = {123456},
year = {2018},
date = {2018-01-01},
journal = {Aircraft Engineering and Aerospace Technology},
volume = {90},
number = {4},
publisher = {Emeraldinsight},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
|
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 @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.mdpi.com/2226-4310/5/2/47/htm},
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. |
2017
|
Charbonnier, D; Vos, J B; Prakasha, P S; Mirzoyan, A; Savelyev, A; Della Vecchia, P Low Speed Take-Off Aerodynamic Analysis. Conference Paper 272 , 6th CEAS Air & Space Conference Aerospace Europe , Bucharest, Romania, 2017. Abstract | Links | BibTeX @conference{ Charbonnier2017_40 ,
title = {Low Speed Take-Off Aerodynamic Analysis.},
author = {D. Charbonnier and J.B. Vos and P.S. Prakasha and A. Mirzoyan and A. Savelyev and P. {Della Vecchia}},
url = {https://www.agile-project.eu/cloud/index.php/s/KwSv2XqEtkvXrBm},
year = {2017},
date = {2017-10-01},
volume = {Paper 272},
address = {Bucharest, Romania},
organization = {6th CEAS Air & Space Conference Aerospace Europe ,},
abstract = {In the frame of the EU funded H2020 project AGILE (Aircraft 3rd Generation MDO for Innovative Collab- oration of Heterogeneous Teams of Experts) detailed CFD simulations were made to analyze the high lift system of an optimized regional aircraft. The paper presents shortly how the different components of the aircraft were obtained and integrated in a model suitable to perform the simulations. High-fidelity RANS (Reynolds-Averaged Navier-Stokes) CFD calculations were carried out, with a focus on take-off conditions, and aerodynamic coefficients as well as flow field distributions were extracted. The results are discussed, and point out in one hand the reliability of high-fidelity CFD simulations to highlight detailed flow phenomena like flow separations, and in another hand the importance to consider low speed flow regimes (take-off or landing) in an aircraft design and optimization process.},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
In the frame of the EU funded H2020 project AGILE (Aircraft 3rd Generation MDO for Innovative Collab- oration of Heterogeneous Teams of Experts) detailed CFD simulations were made to analyze the high lift system of an optimized regional aircraft. The paper presents shortly how the different components of the aircraft were obtained and integrated in a model suitable to perform the simulations. High-fidelity RANS (Reynolds-Averaged Navier-Stokes) CFD calculations were carried out, with a focus on take-off conditions, and aerodynamic coefficients as well as flow field distributions were extracted. The results are discussed, and point out in one hand the reliability of high-fidelity CFD simulations to highlight detailed flow phenomena like flow separations, and in another hand the importance to consider low speed flow regimes (take-off or landing) in an aircraft design and optimization process. |
Zhang, M; Jungo, A; Bartoli, N Disciplinary Data Fusion for Multi-Fidelity Aerodynamic Application. Conference Paper 953 , 6th CEAS Air & Space Conference Aerospace Europe , Bucharest, Romania, 2017. Abstract | Links | BibTeX @conference{ Zhang2017_68 ,
title = {Disciplinary Data Fusion for Multi-Fidelity Aerodynamic Application.},
author = {M. Zhang and A. Jungo and N. Bartoli},
url = {https://www.agile-project.eu/cloud/index.php/s/OlTdWacuqwKaFCo},
year = {2017},
date = {2017-10-01},
volume = {Paper 953},
address = {Bucharest, Romania},
organization = {6th CEAS Air & Space Conference Aerospace Europe ,},
abstract = {This paper presents some multi-fidelity activities in the field of aerodynamic in the ongoing EU-funded re- search project AGILE. Different computation tools relative to different level of fidelity are used in the project and the idea is to combine all the data in a global surrogate model to reduce the computational time in an optimization process for instance. The paper focuses on the data fusion tool embedded in the AGILE frame- work with the choice of the surrogate models, the choice of the tool’s fidelity and the choice of the sampling points via an iterative process. The paper will detail the different steps of the proposed approach to set up and operate the data fusion service proposed to the AGILE partners.},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
This paper presents some multi-fidelity activities in the field of aerodynamic in the ongoing EU-funded re- search project AGILE. Different computation tools relative to different level of fidelity are used in the project and the idea is to combine all the data in a global surrogate model to reduce the computational time in an optimization process for instance. The paper focuses on the data fusion tool embedded in the AGILE frame- work with the choice of the surrogate models, the choice of the tool’s fidelity and the choice of the sampling points via an iterative process. The paper will detail the different steps of the proposed approach to set up and operate the data fusion service proposed to the AGILE partners. |
Berdajs, D; Mosbahi, S; Ferrari, E; Charbonnier, D; von Segesser, L K Aortic Valve Pathology as a Predictive Factor for Acute Aortic Dissection Journal Article The Annals of thoracic surgery, 104 (4), pp. 1340-1348, 2017. Abstract | Links | BibTeX @article{ Berdajs2017_73 ,
title = {Aortic Valve Pathology as a Predictive Factor for Acute Aortic Dissection},
author = {D. Berdajs and S. Mosbahi and E. Ferrari and D. Charbonnier and L.K. {von Segesser}},
url = {https://www.annalsthoracicsurgery.org/article/S0003-4975(17)30400-9/abstract},
doi = {https://doi.org/10.1016/j.athoracsur.2017.02.076},
year = {2017},
date = {2017-06-01},
journal = {The Annals of thoracic surgery},
volume = {104},
number = {4},
pages = {1340-1348},
publisher = {Elsevier},
abstract = {In this study, the effect of aortic valve (AV) pathology on local hemodynamic conditions was evaluated as a potential trigger for the onset of acute type A and B aortic dissection.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
In this study, the effect of aortic valve (AV) pathology on local hemodynamic conditions was evaluated as a potential trigger for the onset of acute type A and B aortic dissection. |
Vos, J B; Charbonnier, D; Ludwig, T; Merazzi, S; Gehri, A; Stephani, P Recent Developments on Fluid Structure Interaction in the Navier Stokes Multi Block (NSMB) CFD solver Conference AIAA-2017-4458 , AIAA Aviation 2017 , Denver, 2017. Links | BibTeX @conference{ Vos2017_101 ,
title = {Recent Developments on Fluid Structure Interaction in the Navier Stokes Multi Block (NSMB) CFD solver},
author = {J.B. Vos and D. Charbonnier and T. Ludwig and S. Merazzi and A. Gehri and P. Stephani},
url = {https://cfse.ch/wp-content/uploads/2019/05/AIAA-2017-4458.pdf},
year = {2017},
date = {2017-06-01},
volume = {AIAA-2017-4458},
address = {Denver},
organization = {AIAA Aviation 2017 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Berdajs, D; Mosbahi, S; Strano, F; Forro, Z; Burki, M; von Segesser, L K Impact of synthetic elements on aortic root haemodynamics: computed fluid dynamics of aortic root reconstruction and valve reimplantation Journal Article European Journal of Cardio-thoracic Surgery, 51 (3), pp. 432-441, 2017. Abstract | Links | BibTeX @article{ Berdajs2017_137 ,
title = {Impact of synthetic elements on aortic root haemodynamics: computed fluid dynamics of aortic root reconstruction and valve reimplantation},
author = {D. Berdajs and S. Mosbahi and F. Strano and Z. Forro and M. Burki and L.K. {von Segesser}},
url = {https://academic.oup.com/ejcts/article/51/3/432/2738865},
doi = {https://doi.org/10.1093/ejcts/ezw347},
year = {2017},
date = {2017-03-01},
journal = {European Journal of Cardio-thoracic Surgery},
volume = {51},
number = {3},
pages = {432-441},
publisher = {Oxford University Press },
abstract = {The aim was to evaluate the impact of the aortic valve reimplantation (David) and of the aortic root (AoR) remodelling (Yacoub) on the AoR haemodynamics.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
The aim was to evaluate the impact of the aortic valve reimplantation (David) and of the aortic root (AoR) remodelling (Yacoub) on the AoR haemodynamics. |
Gastaldi, Alessandro Development of a Double-Lattice Method Program for Aeroelastic Analysis in Conceptual Aircraft Design. Masters Thesis EPFL – CFS Engineering, 2017. Links | BibTeX @mastersthesis{ Gastaldi2017_102 ,
title = {Development of a Double-Lattice Method Program for Aeroelastic Analysis in Conceptual Aircraft Design.},
author = {Alessandro Gastaldi},
url = {https://www.agile-project.eu/cloud/index.php/s/5G0cq7M2jHtUgMR},
year = {2017},
date = {2017-01-01},
school = {EPFL – CFS Engineering},
keywords = {},
pubstate = {published},
tppubtype = {mastersthesis}
}
|
2016
|
Zhang, M; Rizzi, A; Jungo, A; Vos, J B Automated Meshing and Data Fusion applied to create Aerodataset for AGILE DC-1 Configuration. Conference 6th EASN Workshop , Porto, Portugal, 2016. Links | BibTeX @conference{ Zhang2016_93 ,
title = {Automated Meshing and Data Fusion applied to create Aerodataset for AGILE DC-1 Configuration.},
author = {M. Zhang and A. Rizzi and A. Jungo and J.B. Vos},
url = {https://www.agile-project.eu/cloud/index.php/s/RDT70j9a9ye6oR5},
year = {2016},
date = {2016-10-01},
address = {Porto, Portugal},
organization = {6th EASN Workshop ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Jungo, A; Vos, J B; Zhang, M; Rizzi, A Benchmarkig New CEASIOM with CPACS Adoption for Aerodynamic Analysis and Flight Simulation. Conference 6th SCAD & READ Workshop , Warsaw, Poland, 2016. Links | BibTeX @conference{ Jungo2016_91 ,
title = {Benchmarkig New CEASIOM with CPACS Adoption for Aerodynamic Analysis and Flight Simulation.},
author = {A. Jungo and J.B. Vos and M. Zhang and A. Rizzi},
url = {https://www.agile-project.eu/cloud/index.php/s/azueBN1q6vanpll},
year = {2016},
date = {2016-09-01},
address = {Warsaw, Poland},
organization = {6th SCAD & READ Workshop ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Berdajs, D; Mosbahi, S; Forro, Z; Gerber, C; Burki, M; von Segesser, L K Aortic root haemodynamics following David procedure: numerical analysis of 3-dimensional haemodynamics Journal Article European Journal of Cardio-thoracic Surgery, 49 (6), pp. 1588-1598, 2016. Abstract | Links | BibTeX @article{ Berdajs2016_102 ,
title = {Aortic root haemodynamics following David procedure: numerical analysis of 3-dimensional haemodynamics},
author = {D. Berdajs and S. Mosbahi and Z. Forro and C. Gerber and M. Burki and L.K. {von Segesser}},
url = {https://academic.oup.com/ejcts/article/49/6/1588/2197382},
doi = {https://doi.org/10.1093/ejcts/ezv427},
year = {2016},
date = {2016-06-01},
journal = {European Journal of Cardio-thoracic Surgery},
volume = {49},
number = {6},
pages = {1588-1598},
publisher = {Oxford University Press },
abstract = {The aim was to determine 3-dimensional (3D) geometrical deformation of the aortic root (AoR) following the David procedure in order to evaluate local haemodynamical conditions of individual AoR elements.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
The aim was to determine 3-dimensional (3D) geometrical deformation of the aortic root (AoR) following the David procedure in order to evaluate local haemodynamical conditions of individual AoR elements. |
Berdajs, D; Mosbahi, S; Forro, Z; Gerber, C; Ferrari, E; Charbonnier, D; von Segesser, L K Numerical analysis of the 3-dimensional aortic root morphology during the cardiac cycle Journal Article European Journal of Cardio-thoracic Surgery, 49 (4), pp. 1213-1221, 2016. Abstract | Links | BibTeX @article{ Berdajs2016_87 ,
title = {Numerical analysis of the 3-dimensional aortic root morphology during the cardiac cycle},
author = {D. Berdajs and S. Mosbahi and Z. Forro and C. Gerber and E. Ferrari and D. Charbonnier and L.K. {von Segesser}},
url = {https://academic.oup.com/ejcts/article/49/4/1213/2465325},
doi = {https://doi.org/10.1093/ejcts/ezv295},
year = {2016},
date = {2016-04-01},
journal = {European Journal of Cardio-thoracic Surgery},
volume = {49},
number = {4},
pages = {1213-1221},
publisher = {Oxford University Press },
abstract = {The aim was to define the 3-dimensional (3D) geometrical changes of the aortic root and to determine the local shear stress profile of aortic root elements during the cardiac cycle.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
The aim was to define the 3-dimensional (3D) geometrical changes of the aortic root and to determine the local shear stress profile of aortic root elements during the cardiac cycle. |
Vos, J B; Bourgoing, A; Soler, J Earth re-entry capsule CFS simulations taking into account surface roughness and mass injection at the wall Journal Article "Int. J. of Aerodynamics ", 5 (1), 2016. Links | BibTeX @article{ Vos2016_107 ,
title = {Earth re-entry capsule CFS simulations taking into account surface roughness and mass injection at the wall},
author = {J.B. Vos and A. Bourgoing and J. Soler},
url = {https://doi.org/10.1504/IJAD.2015.074622},
year = {2016},
date = {2016-02-01},
journal = {"Int. J. of Aerodynamics "},
volume = {5},
number = {1},
publisher = {Inderscience},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
|
Hoarau, Y; Pena, D; Vos, J B; Charbonnier, D; Gehri, A; Braza, M; Deloze, T; Laurendeau, E Recent Developments of the Navier Stokes Multi Block (NSMB) CFD solver Conference AIAA-2016-2056 , AIAA Scitec 2016 , San Diego, 2016. Links | BibTeX @conference{ Hoarau2016_70 ,
title = {Recent Developments of the Navier Stokes Multi Block (NSMB) CFD solver},
author = {Y. Hoarau and D. Pena and J.B. Vos and D. Charbonnier and A. Gehri and M. Braza and T. Deloze and E. Laurendeau},
url = {https://cfse.ch/wp-content/uploads/2019/05/AIAA-2016-2056.pdf},
year = {2016},
date = {2016-01-01},
volume = {AIAA-2016-2056},
address = {San Diego},
organization = {AIAA Scitec 2016 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Tomac, M; Rizzi, A; Charbonnier, D; Vos, J B; Jirasek, A; Winkler, Pengand S-H A; Allen, A; Wissocq, G; Puigt, G; Dandois, J; Abarca-Lopez, R Unsteady Aero-Loads from Vortices Shed on A320 Landing Gear Door: CFD compared to flight tests Conference AIAA-2016-0803 , AIAA Scitech 2016 , San Diego, 2016. Links | BibTeX @conference{ Tomac2016_94 ,
title = {Unsteady Aero-Loads from Vortices Shed on A320 Landing Gear Door: CFD compared to flight tests},
author = {M. Tomac and A. Rizzi and D. Charbonnier and J.B. Vos and A. Jirasek and S-H. Pengand A. Winkler and A. Allen and G. Wissocq and G. Puigt and J. Dandois and R. Abarca-Lopez},
url = {https://cfse.ch/wp-content/uploads/2019/05/AIAA-2016-0803.pdf},
year = {2016},
date = {2016-01-01},
volume = {AIAA-2016-0803},
address = {San Diego},
organization = {AIAA Scitech 2016 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Rizzi, A; Zhang, M; Bisson, F; Nadarajah, S Comparative Study of Two Optimization Frameworks Applied to Case III: Induced-Drag Minimization Conference AIAA-2016-1296 , AIAA Scitech 2016 , San Diego, 2016. Links | BibTeX @conference{ Rizzi2016_95 ,
title = {Comparative Study of Two Optimization Frameworks Applied to Case III: Induced-Drag Minimization},
author = {A. Rizzi and M. Zhang and F. Bisson and S. Nadarajah},
url = {https://doi.org/10.2514/6.2016-1296},
year = {2016},
date = {2016-01-01},
volume = {AIAA-2016-1296},
address = {San Diego},
organization = {AIAA Scitech 2016 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
2015
|
Berdajs, D; Mosbahi, S; Vos, J; Charbonnier, D; Hullin, R; von Segesser, L K Fluid dynamics simulation of right ventricular outflow tract oversizing Journal Article Interactive Cardiovascular and Thoracic Surgery, 21 (2), pp. 176-182, 2015. Abstract | Links | BibTeX @article{ Berdajs2015_71 ,
title = {Fluid dynamics simulation of right ventricular outflow tract oversizing},
author = {D. Berdajs and S. Mosbahi and J. Vos and D. Charbonnier and R. Hullin and L.K. {von Segesser}},
url = {https://academic.oup.com/icvts/article/21/2/176/766587},
doi = {https://doi.org/10.1093/icvts/ivv108},
year = {2015},
date = {2015-08-01},
journal = {Interactive Cardiovascular and Thoracic Surgery},
volume = {21},
number = {2},
pages = {176-182},
publisher = {Oxford University Press },
abstract = {Repair of the right ventricular outflow tract (RVOT) in paediatric cardiac surgery remains challenging due to the high reoperation rate. Intimal hyperplasia and consequent arteriosclerosis is one of the most important limitation factors for graft durability. Since local shear stress and pressure are predictive elements for intimal hyperplasia and wall degeneration, we sought to determine in an oversized 12-mm RVOT model, with computed fluid dynamics simulation, the local haemodynamical factors that may explain intimal hyperplasia. This was done with the aim of identifying the optimal degree of oversizing for a 12-mm native RVOT.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
Repair of the right ventricular outflow tract (RVOT) in paediatric cardiac surgery remains challenging due to the high reoperation rate. Intimal hyperplasia and consequent arteriosclerosis is one of the most important limitation factors for graft durability. Since local shear stress and pressure are predictive elements for intimal hyperplasia and wall degeneration, we sought to determine in an oversized 12-mm RVOT model, with computed fluid dynamics simulation, the local haemodynamical factors that may explain intimal hyperplasia. This was done with the aim of identifying the optimal degree of oversizing for a 12-mm native RVOT. |
Berdajs, D; Mosbahi, S; Charbonnier, D; Hullin, R; von Segesser, L K Analysis of flow dynamics in right ventricular outflow tract Journal Article Journal of Surgical Research, 197 (1), pp. 50-57, 2015. Abstract | Links | BibTeX @article{ Berdajs2015_60 ,
title = {Analysis of flow dynamics in right ventricular outflow tract},
author = {D. Berdajs and S. Mosbahi and D. Charbonnier and R. Hullin and L.K. {von Segesser}},
url = {https://www.journalofsurgicalresearch.com/article/S0022-4804(15)00220-6/abstract},
doi = {https://doi.org/10.1016/j.jss.2015.03.001},
year = {2015},
date = {2015-07-01},
journal = {Journal of Surgical Research},
volume = {197},
number = {1},
pages = {50-57},
publisher = {Elsevier},
abstract = {The mechanism behind early graft failure after right ventricular outflow tract (RVOT) reconstruction is not fully understood. Our aim was to establish a three-dimensional computational fluid dynamics (CFD) model of RVOT to investigate the hemodynamic conditions that may trigger the development of intimal hyperplasia and arteriosclerosis.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
The mechanism behind early graft failure after right ventricular outflow tract (RVOT) reconstruction is not fully understood. Our aim was to establish a three-dimensional computational fluid dynamics (CFD) model of RVOT to investigate the hemodynamic conditions that may trigger the development of intimal hyperplasia and arteriosclerosis. |
Charbonnier, D; Vos, J B; Clopeau, E; Ferracina, L; Maraffa, L MarcoPolo-R ERC Dynamic Stability Characterization: Computational Campaign Conference ESA ATD , Lisbon, 2015. Links | BibTeX @conference{ Charbonnier2015_74 ,
title = {MarcoPolo-R ERC Dynamic Stability Characterization: Computational Campaign},
author = {D. Charbonnier and J.B. Vos and E. Clopeau and L. Ferracina and L. Maraffa},
url = {https://www.researchgate.net/publication/275638548_MarcoPolo-R_ERC_Dynamic_Stability_Characterization_Computational_Campaign},
year = {2015},
date = {2015-03-01},
address = {Lisbon},
organization = {ESA ATD ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
2014
|
Mosbahi, S; Mickaily-Huber, E; Charbonnier, D; Hullin, R; Burki, M; Ferrari, E; von Segesser, L K; Berdajs, D Computational fluid dynamics of the right ventricular outflow tract and of the pulmonary artery: a bench model of flow dynamics Journal Article Interactive Cardiovascular and Thoracic Surgery, 19 (4), pp. 611-616, 2014. Abstract | Links | BibTeX @article{ Mosbahi2014_127 ,
title = {Computational fluid dynamics of the right ventricular outflow tract and of the pulmonary artery: a bench model of flow dynamics},
author = {S. Mosbahi and E. Mickaily-Huber and D. Charbonnier and R. Hullin and M. Burki and E. Ferrari and L.K. {von Segesser} and D. Berdajs},
url = {https://academic.oup.com/icvts/article/19/4/611/765319},
doi = {https://doi.org/10.1093/icvts/ivu202},
year = {2014},
date = {2014-10-01},
journal = {Interactive Cardiovascular and Thoracic Surgery},
volume = {19},
number = {4},
pages = {611-616},
publisher = {Oxford University Press },
abstract = {The reconstruction of the right ventricular outflow tract (RVOT) with valved conduits remains a challenge. The reoperation rate at 5 years can be as high as 25% and depends on age, type of conduit, conduit diameter and principal heart malformation. The aim of this study is to provide a bench model with computer fluid dynamics to analyse the haemodynamics of the RVOT, pulmonary artery, its bifurcation, and left and right pulmonary arteries that in the future may serve as a tool for analysis and prediction of outcome following RVOT reconstruction.},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
The reconstruction of the right ventricular outflow tract (RVOT) with valved conduits remains a challenge. The reoperation rate at 5 years can be as high as 25% and depends on age, type of conduit, conduit diameter and principal heart malformation. The aim of this study is to provide a bench model with computer fluid dynamics to analyse the haemodynamics of the RVOT, pulmonary artery, its bifurcation, and left and right pulmonary arteries that in the future may serve as a tool for analysis and prediction of outcome following RVOT reconstruction. |
2013
|
Vos, J B; Sanchi, S; Gehri, A Drag Prediction Workshop 4 Results Using Different Grids Including Near-Field/Far-Field Drag Analysis Journal Article "Journal of Aircraft ", 50 (5), 2013. Links | BibTeX @article{ Vos2013_101 ,
title = {Drag Prediction Workshop 4 Results Using Different Grids Including Near-Field/Far-Field Drag Analysis},
author = {J.B. Vos and S. Sanchi and A. Gehri},
url = {https://doi.org/10.2514/1.C032161},
year = {2013},
date = {2013-10-01},
journal = {"Journal of Aircraft "},
volume = {50},
number = {5},
publisher = {AIAA},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
|
2012
|
Di Clemente, M; Trifoni, E; Walpot, L; Thoemel, J; Vos, J B; Guelhan, A; Thiele, T; Pereira, C Aerothermal Rebuilding of Plasma Wind Tunnel Tests on the EXPERT Capsule Open Flap Conference AIAA-2012-3003 , AIAA Aviation 2012 , New Orleans, 2012. Links | BibTeX @conference{ Di2012_82 ,
title = {Aerothermal Rebuilding of Plasma Wind Tunnel Tests on the EXPERT Capsule Open Flap},
author = {M. {Di Clemente} and E. Trifoni and L. Walpot and J. Thoemel and J.B. Vos and A. Guelhan and T. Thiele and C. Pereira},
url = {https://doi.org/10.2514/6.2012-3003},
year = {2012},
date = {2012-06-01},
volume = {AIAA-2012-3003},
address = {New Orleans},
organization = {AIAA Aviation 2012 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
2011
|
Rizzi, A W; Eliasson, P; Goetzendorf-Grabowski, T; Vos, J B; Zhang, M; Richardson, T S Design of a canard configured TransCruiser using CEASIOM Journal Article "Progress in Aerospace Sciences ", 47 (8), 2011. Links | BibTeX @article{ Rizzi2011_56 ,
title = {Design of a canard configured TransCruiser using CEASIOM},
author = {A.W. Rizzi and P. Eliasson and T. Goetzendorf-Grabowski and J.B. Vos and M. Zhang and T.S. Richardson},
url = {https://doi.org/10.1016/j.paerosci.2011.08.011},
year = {2011},
date = {2011-11-01},
journal = {"Progress in Aerospace Sciences "},
volume = {47},
number = {8},
publisher = {Elsevier},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
|
Guillaume, M; Gehri, A; Stephani, P; Vos, J B; Mandanis, G F/A-18 vertical buffeting calculations using unsteady fluid structure interaction Journal Article "The Aeronautical Journal ", 115 (1167), 2011. Links | BibTeX @article{ Guillaume2011_82 ,
title = {F/A-18 vertical buffeting calculations using unsteady fluid structure interaction},
author = {M. Guillaume and A. Gehri and P. Stephani and J.B. Vos and G. Mandanis},
url = {https://doi.org/10.1017/S0001924000005777},
year = {2011},
date = {2011-05-01},
journal = {"The Aeronautical Journal "},
volume = {115},
number = {1167},
publisher = {Cambridge University Press},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
|
2010
|
Guillaume, M; Gehri, A; Stephani, P; Vos, J B; Mandanis, G Fluid Structure Interaction Simulation on the F/A-18 Vertical Tail Conference AIAA-2010-4613 , AIAA Aviation 2010 , Chicago, 2010. Links | BibTeX @conference{ Guillaume2010_66 ,
title = {Fluid Structure Interaction Simulation on the F/A-18 Vertical Tail},
author = {M. Guillaume and A. Gehri and P. Stephani and J.B. Vos and G. Mandanis},
url = {https://cfse.ch/wp-content/uploads/2019/05/AIAA-2010-4613.pdf},
year = {2010},
date = {2010-06-01},
volume = {AIAA-2010-4613},
address = {Chicago},
organization = {AIAA Aviation 2010 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
Vos, J B; Sanchi, S; Gehri, A DPW4 Results Using Different Grids Including Near-Field/Far-Field Drag Analysis Conference AIAA-2010-4552 , AIAA Aviation 2010 , Chicago, 2010. Links | BibTeX @conference{ Vos2010_79 ,
title = {DPW4 Results Using Different Grids Including Near-Field/Far-Field Drag Analysis},
author = {J.B. Vos and S. Sanchi and A. Gehri},
url = {https://cfse.ch/wp-content/uploads/2019/05/AIAA-2010-4552.pdf},
year = {2010},
date = {2010-06-01},
volume = {AIAA-2010-4552},
address = {Chicago},
organization = {AIAA Aviation 2010 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|
2002
|
Vos, J B; Rizzi, A W; Darracq, D; Hirschel, E H Navier Stokes solvers in European Aircraft Design Journal Article "Progress in Aerospace Sciences ", 38 (8), 2002. Links | BibTeX @article{ Vos2002_49 ,
title = {Navier Stokes solvers in European Aircraft Design},
author = {J.B. Vos and A.W. Rizzi and D. Darracq and E.H. Hirschel},
url = {https://doi.org/10.1016/S0376-0421(02)00050-7},
year = {2002},
date = {2002-11-01},
journal = {"Progress in Aerospace Sciences "},
volume = {38},
number = {8},
publisher = {Elsevier},
keywords = {},
pubstate = {published},
tppubtype = {article}
}
|
1998
|
Vos, J B; Rizzi, A W; Corjon, A; Chaput, E; Soinne, E Recent Advances in Aerodynamics inside the NSMB (Navier Stokes Multi Block) Consortium Conference AIAA-1998-0225 , AIAA Scitech 1998 , Reno, 1998. Links | BibTeX @conference{ Vos1998_86 ,
title = {Recent Advances in Aerodynamics inside the NSMB (Navier Stokes Multi Block) Consortium},
author = {J.B. Vos and A.W. Rizzi and A. Corjon and E. Chaput and E. Soinne},
url = {https://doi.org/10.2514/6.1998-225},
year = {1998},
date = {1998-01-01},
volume = {AIAA-1998-0225},
address = {Reno},
organization = {AIAA Scitech 1998 ,},
keywords = {},
pubstate = {published},
tppubtype = {conference}
}
|