Algorithmic Differentiation for adjoint sensitivity calculation in plasma edge codes
S Carli, L Hascoët, W Dekeyser… - Journal of Computational …, 2023 - Elsevier
In the framework of fusion energy research, divertor design and model calibration based on
plasma edge codes currently rely either on manual iterative tuning of parameters, or …
plasma edge codes currently rely either on manual iterative tuning of parameters, or …
Goal oriented mesh adaptation using total derivative of aerodynamic functions with respect to mesh coordinates–With applications to Euler flows
In aeronautical CFD, engineers require accurate predictions of the forces and moments but
they are less concerned with the accuracy of the detailed flow-field. Hence, the so-called …
they are less concerned with the accuracy of the detailed flow-field. Hence, the so-called …
Bayesian maximum a posteriori‐estimation of κ turbulence model parameters using algorithmic differentiation in SOLPS‐ITER
S Carli, W Dekeyser, M Blommaert… - … to Plasma Physics, 2022 - Wiley Online Library
Radial anomalous diffusion coefficients are among the largest sources of uncertainty in
mean‐field plasma‐edge codes such as SOLPS‐ITER. These coefficients are machine …
mean‐field plasma‐edge codes such as SOLPS‐ITER. These coefficients are machine …
A data-driven scalable MDO problem to compare MDO formulations
M De Lozzo, F Gallard, A Gazaix… - AIAA AVIATION 2021 …, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-3053. vid Optimizing a
multidisciplinary system may not be straighforward because of the dimension of both …
multidisciplinary system may not be straighforward because of the dimension of both …
Calcul de la sensibilité d'ordre deux d'une observation aérodynamique
L Martin, G Roge - ESAIM: Proceedings, 2009 - esaim-proc.org
This paper outlines a new formulation for Hessian calculation for a functional of interest for
aerodynamic applications with regards to shape parameters. An analysis of the order of the …
aerodynamic applications with regards to shape parameters. An analysis of the order of the …
Computational and Experimental Assessment of Models for the First AIAA Sonic Boom Prediction Workshop Using Adaptive High Fidelity CFD methods
F Dagrau, A Loseille, I Salah El Din - 32nd AIAA Applied Aerodynamics …, 2014 - arc.aiaa.org
ITH the surge of worldwide projects on the feasibility of an environmentally compliant
supersonic business jet1, an accurate sonic boom computational process is paramount for …
supersonic business jet1, an accurate sonic boom computational process is paramount for …
Qualification of numerical simulations by anisotropic mesh adaptation
M Nguyen-Dinh - 2014 - theses.hal.science
Numerical simulation is widely used for the assessment of aircraft aerodynamic
performances and shape optimizations. Hence the objective of these simulations is often to …
performances and shape optimizations. Hence the objective of these simulations is often to …
NATURAL LAMINAR FLOW HIGH ASPECT RATIO WING SHAPE OPTIMIZATION USING A DISCRETE ADJOINT APPROACH
G Rogé, F Billard, G Laruellle, S Kleinveld, G Sporschill - nextair-project.eu
Natural Laminar Flow (NLF) High Aspect Ratio Wing (HARW) is one of the most promising
ways to dramatically reduce the carbon footprint of Business Jets aircrafts. The aim of our …
ways to dramatically reduce the carbon footprint of Business Jets aircrafts. The aim of our …
Résolution des équations de Navier-Stokes linéarisées pour l'aéroélasticité, l'optimisation de forme et l'aéroacoustique
A Bissuel - 2018 - pastel.hal.science
Les équations de Navier-Stokes linéarisées sont utilisées dans l'industrie aéronautique pour
l'optimisation de forme aérodynamique, l'aéroélasticité et l'aéroacoustique. Deux axes ont …
l'optimisation de forme aérodynamique, l'aéroélasticité et l'aéroacoustique. Deux axes ont …
Shape optimization for greener aircraft: the Dassault Aviation vision and perspectives
G Rogé, S Kleiveld, X Loyatho… - ECCOMAS Congress, 2016 - eccomas2016.org
ABSTRACT The ACARE roadmap beyond 2020 [1] estimates that new aircraft concepts and
airframe aerodynamic improvements could together lead to 30% of fuel burn reductions until …
airframe aerodynamic improvements could together lead to 30% of fuel burn reductions until …