C Kolokotronis, BC Vermeire - Computers & Fluids, 2024 - Elsevier
This work introduces two new non-dimensional gradient-based adaptation indicators for feature-based polynomial adaptation with high-order unstructured methods when used for …
Performing industrial scale incompressible Large Eddy Simulation (LES) remains particularly challenging due to computational cost limitations. Recently, the Entropically …
D Doehring, GJ Gassner, M Torrilhon - Journal of Scientific Computing, 2024 - Springer
A novel optimization procedure for the generation of stability polynomials of stabilized explicit Runge–Kutta methods is devised. Intended for semidiscretizations of hyperbolic …
We investigate the feasibility of gradient-free aeroacoustic shape optimization using the flux reconstruction (FR) approach to study two-dimensional flow at low Reynolds numbers. The …
The paper is devoted to the parametric stability optimization of explicit Runge–Kutta methods with higher-order derivatives. The key feature of these methods is the dependence …
In this paper, we generate optimal Runge–Kutta stability polynomials for several finite- volume spatial discretizations. From these stability polynomials we generate Butcher …
We present an aeroacoustic shape optimization framework that relies on high-order Flux Reconstruction (FR) spatial discretization, the gradient-free Mesh Adaptive Direct Search …
M Hamedi, B Vermeire - arXiv preprint arXiv:2501.05709, 2025 - arxiv.org
This study presents an aeroacoustic shape optimization framework that integrates a Flux Reconstruction (FR) spatial discretization, Large Eddy Simulation (LES), Ffowcs-Williams …
In this paper, we validate a previously proposed highorder method for simulating unsteady flows for a helicopter rotor in hover. To demonstrate the performance and efficiency of this …