output
20122025
most citedMutation++: MUlticomponent Thermodynamic And Transport properties for IONized gases in C++

176 citations

Showing 2022Show all

11 papers · 1 filter

physics.flu-dyn2022★ 25 cited

Experimental analysis of heat and mass transfer in non-isothermal sloshing using a model-based inverse method

Pedro Marques, Alessia Simonini, Laura Peveroni +1

Nonisothermal liquid sloshing in partially filled reservoirs can significantly enhance heat and mass transfer between liquid and ullage gasses. This can result in large temperature…

physics.flu-dyn2022★ 13 cited

A Robust Data-Driven Model for Flapping Aerodynamics under different hovering kinematics

Andre Calado, Romain Poletti, Lilla K. Koloszar +1

Flapping Wing Micro Air Vehicles (FWMAV) are highly manoeuvrable, bio-inspired drones that can assist in surveys and rescue missions. Flapping wings generate various unsteady lift…

physics.flu-dyn2022★ 19 cited

A 1D Model for the Unsteady Gas Dynamics of Ejectors

Jan Van den Berghe, Bruno R. B. Dias, Yann Bartosiewicz +1

We propose a 1D unsteady model for supersonic single-phase ejectors. The model treats an ejector as a pipe network with two inputs and one output and combines a 1D gas dynamics for…

physics.flu-dyn2022★ 15 cited

Effect of inertia on the dynamic contact angle in oscillating menisci

Domenico Fiorini, Miguel Alfonso Mendez, Alessia Simonini +2

The contact angle between a gas-liquid interface and a solid surface is a function of the dynamic conditions of the contact line. Classic steady correlations link the contact angle…

physics.flu-dyn2022★ 49 cited

Linear and Nonlinear Dimensionality Reduction from Fluid Mechanics to Machine Learning

Miguel A. Mendez

Dimensionality reduction is the essence of many data processing problems, including filtering, data compression, reduced-order modeling and pattern analysis. While traditionally ta…

physics.flu-dyn2022★ 10 cited

Data-driven modeling of hypersonic reentry flow with heat and mass transfer

Leonidas Gkimisis, Bruno Ricardo Barros Dias, James B. Scoggins +3

The entry phase constitutes a design driver for aerospace systems that include such a critical step. This phase is characterized by hypersonic flows encompassing multiscale phenome…