Rotorcraft blade-vortex interaction noise prediction using the Lattice-Boltzmann method
Sign Up to like & getrecommendations! Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.03.029
Abstract: Abstract The aim of this paper is to assess the accuracy, capabilities and computational performances of the Lattice-Boltzmann/Very Large Eddy Simulation Method to predict the unsteady aerodynamic loads, the rotor wake development and the noise… read more here.
Keywords: lattice boltzmann; vortex interaction; method; noise ... See more keywords
Two-dimensional and three-dimensional numerical simulations of cycloidal propellers in hover
Sign Up to like & getrecommendations! Published in 2018 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
DOI: 10.1177/0954410016660218
Abstract: The cycloidal propellers for micro aerial vehicle scale cyclocopter in hovering status were studied in this paper based on the URANs solver using 2D, 2.5D, 3D half blade and 3D full blade model. The results… read more here.
Keywords: blade; vortex interactions; blade vortex; model ... See more keywords