From the 1 of 100 papers with an AI index.
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- Trieste Astronomical ObservatoryIT16 papers
- University of BolognaIT14 papers
- Scuola Internazionale Superiore di Studi AvanzatiIT13 papers
- Institute for Fundamental Physics of the UniverseIT11 papers
- National Institute for AstrophysicsIT11 papers
- Centre National de la Recherche ScientifiqueFR10 papers
- Istituto Nazionale di Fisica Nucleare, Sezione di TriesteIT10 papers
- University of Milano-BicoccaIT10 papers
- University of TurinIT9 papers
- Istituto Nazionale di Fisica Nucleare, Sezione di Milano BicoccaIT8 papers
- Istituto di Radioastronomia di BolognaIT7 papers
- Ludwig-Maximilians-Universität MünchenDE7 papers
8 papers · 1 filter
The Gaia AVU-GSR parallel solver: preliminary studies of a LSQR-based application in perspective of exascale systems
Valentina Cesare, Ugo Becciani, Alberto Vecchiato +6
The Gaia Astrometric Verification Unit-Global Sphere Reconstruction (AVU-GSR) Parallel Solver aims to find the astrometric parameters for 10 stars in the Milky Way, the a…
Quantum median filter for Total Variation image denoising
Simone De Santis, Damiana Lazzaro, Riccardo Mengoni +1
In this new computing paradigm, named quantum computing, researchers from all over the world are taking their first steps in designing quantum circuits for image processing, throug…
On floating point precision in computational fluid dynamics using OpenFOAM
F. Brogi, S. Bnà, G. Boga +3
Thanks to the computational power of modern cluster machines, numerical simulations can provide, with an unprecedented level of details, new insights into fluid mechanics. However,…
Entanglement entropy production in Quantum Neural Networks
Marco Ballarin, Stefano Mangini, Simone Montangero +2
Quantum Neural Networks (QNN) are considered a candidate for achieving quantum advantage in the Noisy Intermediate Scale Quantum computer (NISQ) era. Several QNN architectures have…
Drag reduction on a transonic airfoil
Maurizio Quadrio, Alessandro Chiarini, Jacopo Banchetti +3
Flow control for turbulent skin-friction drag reduction is applied to a transonic airfoil to improve its aerodynamic performance. The study is based on direct numerical simulations…
Unsteadiness characterisation of shock wave/turbulent boundary-layer interaction at moderate Reynolds number
Matteo Bernardini, Giacomo Della Posta, Francesco Salvadore +1
A direct numerical simulation of an oblique shock wave impinging on a turbulent boundary layer at Mach number 2.28 is carried out at moderate Reynolds number, simulating flow condi…