byuflowlab/FLOWUnsteady

An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy

Juliacfdaircraftwind-turbinecomputational-fluid-dynamicsaerodynamicsaeroacousticsacousticsvtolvpmvortex-methodsrotorcraft
This is stars and forks stats for /byuflowlab/FLOWUnsteady repository. As of 04 May, 2024 this repository has 189 stars and 54 forks.

Interactional aerodynamics solver for multirotor aircraft and wind energy FLOWUnsteady is an open-source variable-fidelity framework for unsteady aerodynamics and aeroacoustics based on the reformulated vortex particle method (rVPM). This suite brings together various tools developed by the FLOW Lab at Brigham Young University: Vortex lattice method, strip theory, blade elements, 3D panel method, and rVPM. The suite also integrates an FW-H solver and a BPM code for tonal and...
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