Méthode d'assemblage de maillages recouvrants autour de géométries complexes pour des simulations en aérodynamique compressible
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- Type
- dissertation
- Published
- 2014-10-02
- Cited by
- 3
- References
- 45
- OpenAlex
- https://openalex.org/W57034573
- Semantic Scholar
- https://api.semanticscholar.org/CorpusID:187792598
Keywords
Humanities, Physics, Art
References
- A New Approach to Octree-Based Hexahedral Meshing
- Turbulence Measurements in the Near-Field of a Wingtip Vortex
- Adaptively-refined overlapping grids for the numerical solution of systems of hyperbolic conservation laws
- Overset grid technology development at NASA Ames Research Center
- Adaptive mesh refinement for hyperbolic partial differential equations
- Numerical Simulations of a Wingtip Vortex in the Near Field
- Adaptive spatial partitioning and refinement for overset structured grids
- A flexible grid embedding technique with application to the Euler equations
- Three-Dimensional Inviscid Isolated Rotor Calculations Using Chimera and Automatic Cartesian Partitioning Methods
- Reassessment of the scale-determining equation for advanced turbulence models
- Third‐order Cartesian overset mesh adaptation method for solving steady compressible flows
- Feature-driven Cartesian adaptive mesh refinement for vortex-dominated flows
- Automatic off-body overset adaptive Cartesian mesh method based on an octree approach
- Overture: An Object-Oriented Framework for Overlapping Grid Applications
- Numerical simulation of the integrated space shuttle vehicle in ascent
- Automatic Off-Body Grid Generation for Domains of Arbitrary Size
- Numerical/experimental study of a wingtip vortex in the near field
- Large-Eddy Simulation of a Wing Tip Vortex on Overset Grids
- Computation of GOAHEAD configuration with Chimera assembly
- Moving body overset grid methods for complete aircraft tiltrotor simulations
Cited by
- Validation of a near-body and off-body grid partitioning methodology for aircraft aerodynamic performance prediction
- Development of NOVA Aircraft Configurations for Large Engine Integration Studies
- New CFD capabilities based on intersecting arbitrary polyhedral meshes: P1-conservative interpolations and overset CFD applications
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