20th AIAA Computational Fluid Dynamics Conference · 2011 · 81 citations · 19 references
EngineeringAerospace EngineeringComputational Fluid DynamicsComputational MechanicsFluid DynamicsComputational AerodynamicsConvergence AnalysisFinite Difference MethodsNumerical AnalysisRotordynamics
Conventional nite-di erence methods are the main workhorse of NASA's OVERFLOW code. Recent enhancements in the development, implementation and analysis of simple high-order accurate nite-di erence techniques within OVERFLOW are documented here. Results are presented for simple vortex propagation to demonstrate the salient features of the methods, and more complex three-dimensional rotorcraft ows are used to validate their usefulness in real applications.
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