FLOWUnsteady --- Blown wing
Автор: Ed Alvarez
Загружено: 2020-01-27
Просмотров: 2904
Описание:
Preliminary results of a blown wing simulation capturing rotor-on-wing and wing-on-rotor interactions, where the wing is modeled as a lifting line. Notice that the unsteady loading of the rotors is merely due to the presence of the wing.
FLOWUnsteady is a mixed-fidelity unsteady aerodynamics and aeroacoustics simulator. This suite brings together all the aerodynamics tools developed at BYU's FLOW Lab: Vortex lattice method, strip theory, blade-element momentum, 3D panel method, and viscous vortex particle method. The suite also integrates PSU-WOPWOP (FW-H solver) for aeroacoustic predictions.
FLOWUnsteady solves all rotor-on-rotor, rotor-on-wing, wing-on-rotor, and wing-on-wing interactions encountered by a vehicles along a prescribed maneuver.
• Code: https://github.com/byuflowlab/FLOWUns...
• More projects: http://edoalvarez.com
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