1. A Hybrid Non-Linear Unsteady Vortex Lattice-Vortex Particle Method for Rotor Blades Aerodynamic Simulations
- Author
-
Vincent Proulx-Cabana, Minh Tuan Nguyen, Sebastien Prothin, Guilhem Michon, Eric Laurendeau, Centre National de la Recherche Scientifique - CNRS (FRANCE), Ecole Polytechnique de Montréal (CANADA), Ecole nationale supérieure des Mines d'Albi-Carmaux - IMT Mines Albi (FRANCE), Institut National des Sciences Appliquées de Toulouse - INSA (FRANCE), Institut Supérieur de l'Aéronautique et de l'Espace - ISAE-SUPAERO (FRANCE), Université Toulouse III - Paul Sabatier - UT3 (FRANCE), Département Aérodynamique Energétique et Propulsion - DAEP (Toulouse, France), École Polytechnique de Montréal (EPM), Institut Clément Ader (ICA), Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO)-Institut National des Sciences Appliquées - Toulouse (INSA Toulouse), Institut National des Sciences Appliquées (INSA)-Université de Toulouse (UT)-Institut National des Sciences Appliquées (INSA)-Université de Toulouse (UT)-Université Toulouse III - Paul Sabatier (UT3), Université de Toulouse (UT)-Centre National de la Recherche Scientifique (CNRS)-IMT École nationale supérieure des Mines d'Albi-Carmaux (IMT Mines Albi), Institut Mines-Télécom [Paris] (IMT)-Institut Mines-Télécom [Paris] (IMT), Département Aérodynamique Energétique et Propulsion (DAEP), and Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO)
- Subjects
Fluid Flow and Transfer Processes ,Mechanical Engineering ,Large eddy simulation ,Vortex particle method ,Condensed Matter Physics ,Helicopter aerodynamics ,Physics::Fluid Dynamics ,unsteady vortex lattice method ,Lagrangian method ,vortex particle method ,large eddy simulation ,non-linear viscous-inviscid coupling ,helicopter aerodynamics ,rotor blades ,Mécanique des structures ,Non-linear viscous-inviscid coupling ,[SPI.MECA.STRU]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Structural mechanics [physics.class-ph] ,Rotor blades ,Unsteady vortex lattice method - Abstract
International audience; This study presents a hybrid non-linear unsteady vortex lattice method-vortex particle method (NL UVLM-VPM) to investigate the aerodynamics of rotor blades hovering in and out of ground effect. The method is of interest for the fast aerodynamic prediction of helicopter and smaller rotor blades. UVLM models the vorticity along the rotor blades and near field wakes with panels that are then converted into their equivalent vortex particle representations. The standard Vreman subgrid scale model is incorporated in the context of a large eddy simulation for mesh-free VPM to stabilize the wake development via particle strength exchange (PSE). The computation of the pairwise interactions in the VPM are accelerated using the fast-multipole method. Non-linear UVLM is achieved with a low computational cost viscous-inviscid alpha coupling algorithm through a stripwise 2D Reynolds-averaged Navier–Stokes (RANS) or empirical database. The aerodynamics of the scaled S76 rotor blades in and out of ground effect from the hover prediction workshop is investigated with the proposed algorithm. The results are validated with experimental data and various high-fidelity codes.
- Published
- 2022
- Full Text
- View/download PDF