Application of a lattice Boltzmann method to some challenges related to micro-air vehicles
暂无分享,去创建一个
Nicolas Gourdain | Jean-Marc Moschetta | Sebastien Prothin | Thierry Jardin | Ronan Serre | N. Gourdain | J. Moschetta | S. Prothin | T. Jardin | R. Serré
[1] Orestis Malaspinas,et al. General regularized boundary condition for multi-speed lattice Boltzmann models , 2011 .
[2] Leonhard Kleiser,et al. Large-eddy simulation of vortex breakdown in compressible swirling jet flow , 2008 .
[3] Adam C. DeVoria,et al. Aspect-ratio effects on rotating wings: circulation and forces , 2015, Journal of Fluid Mechanics.
[4] Haibo Dong,et al. Large-Eddy Simulation of the Tip Flow of a Rotor in Hover , 2004 .
[5] I. Mary,et al. Large eddy simulation of vortex breakdown behind a delta wing , 2003 .
[6] L. David,et al. Coriolis effects enhance lift on revolving wings. , 2015, Physical review. E, Statistical, nonlinear, and soft matter physics.
[7] Albert Medina,et al. Leading-edge vortex burst on a low-aspect-ratio rotating flat plate , 2016 .
[8] D. d'Humières,et al. Multiple–relaxation–time lattice Boltzmann models in three dimensions , 2002, Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences.
[9] Daniel J. Bodony,et al. Analysis of sponge zones for computational fluid mechanics , 2006, J. Comput. Phys..
[10] Ugo Piomelli,et al. Reynolds-averaged and wall-modelled large-eddy simulations of impinging jets with embedded azimuthal vortices , 2016 .
[11] Hao Liu,et al. Recent progress in flapping wing aerodynamics and aeroelasticity , 2010 .
[12] Pierre Sagaut,et al. Toward advanced subgrid models for Lattice-Boltzmann-based Large-eddy simulation: Theoretical formulations , 2010, Comput. Math. Appl..
[13] B. Chopard,et al. Lattice Boltzmann Method with regularized non-equilibrium distribution functions , 2005, physics/0506157.
[14] Tim Colonius,et al. A fast lattice Green's function method for solving viscous incompressible flows on unbounded domains , 2015, J. Comput. Phys..
[15] Sebastien Prothin,et al. Aerodynamic Performance of a Hovering Microrotor in Confined Environment , 2017 .
[16] J. W. Kim,et al. Performance and mechanism of sinusoidal leading edge serrations for the reduction of turbulence–aerofoil interaction noise , 2017, Journal of Fluid Mechanics.
[17] Anibal Ollero,et al. Characterization of the Aerodynamic Ground Effect and Its Influence in Multirotor Control , 2017 .
[18] F. Farassat,et al. Theory of Noise Generation From Moving Bodies With an Application to Helicopter Rotors , 1975 .
[19] Joseph F. Horn,et al. Active stabilization of slung loads in high speed flight using cable angle feedback , 2019 .
[20] Scott A. Morton,et al. DES and RANS simulations of delta wing vortical flows , 2002 .
[21] Tim Colonius,et al. A fast immersed boundary method for external incompressible viscous flows using lattice Green's functions , 2016, J. Comput. Phys..
[22] Tim Colonius,et al. Immersed Boundary Lattice Green Function methods for External Aerodynamics , 2017 .
[23] Takaji Inamuro,et al. Lattice Boltzmann methods for moving boundary flows , 2012 .
[24] Sophie Papst,et al. Computational Methods For Fluid Dynamics , 2016 .
[25] Nicolas Gourdain,et al. Lattice Boltzmann simulation and analysis of the turbulent wake of a MAV hovering near the ground , 2016 .
[26] Thomas B. Gatski,et al. A criterion for vortex breakdown , 1987 .
[27] P. Lallemand,et al. Theory of the lattice boltzmann method: dispersion, dissipation, isotropy, galilean invariance, and stability , 2000, Physical review. E, Statistical physics, plasmas, fluids, and related interdisciplinary topics.
[28] Pierre Sagaut,et al. Wall model for large-eddy simulation based on the lattice Boltzmann method , 2014, J. Comput. Phys..
[29] T. O’Doherty,et al. Vortex breakdown: a review , 2001 .
[30] Phillip Joseph,et al. Experimental and numerical investigation of turbulence-airfoil noise reduction using wavy edges , 2013 .
[31] Nicolas Gourdain,et al. Analysis of the Turbulent Wake Generated by a Micro Air Vehicle Hovering near the Ground with a Lattice Boltzmann Method , 2017 .
[32] M. Giles,et al. Viscous-inviscid analysis of transonic and low Reynolds number airfoils , 1986 .
[33] James D. Baeder,et al. Detailed Computational Investigation of a Hovering Microscale Rotor in Ground Effect , 2013 .
[34] Inderjit Chopra,et al. Hover Tests of Micro Aerial Vehicle-Scale Shrouded Rotors, Part I: Performance Characteristics , 2009 .
[35] Hamid Johari,et al. Effects of Leading-Edge Protuberances on Airfoil Performance , 2007 .
[36] C. Rhie,et al. Numerical Study of the Turbulent Flow Past an Airfoil with Trailing Edge Separation , 1983 .
[37] Thierry Jardin,et al. Coriolis effect and the attachment of the leading edge vortex , 2017, Journal of Fluid Mechanics.
[38] M. Dickinson,et al. Rotational accelerations stabilize leading edge vortices on revolving fly wings , 2009, Journal of Experimental Biology.
[39] Laurent David,et al. Root Cutout Effects on the Aerodynamics of a Low-Aspect-Ratio Revolving Wing , 2017 .
[40] Bastien Chopard,et al. Lattice Boltzmann method with regularized pre-collision distribution functions , 2006, Math. Comput. Simul..