Multigrid Acceleration and Chimera Technique for Viscous Flow Past a Hovering Rotor
Author:
Affiliation:
1. Fudan University, 200433 Shanghai, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031069
Reference15 articles.
1. Multigrid acceleration of an upwind Euler method for hovering rotor flows
2. Flowfield of a lifting rotor in hover - A Navier-Stokes simulation
3. Evaluation of a Navier‐Stokes Analysis Method for Hover Performance Prediction
4. Navier-Stokes Analysis of Helicopter Rotor Aerodynamics in Hover and Forward Flight
5. Computational Modeling of Hovering Rotor and Wake Aerodynamics
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1. Acceleration of Euler and RANS solvers via Selective Frequency Damping;Computers & Fluids;2018-04
2. Helicopter Blade-Vortex Interaction Airload and Noise Prediction Using Coupling CFD/VWM Method;Applied Sciences;2017-04-11
3. Efficient Numerical Techniques for Simulating a Rotorcraft Flow Field with Overlapping Grids;AIAA Journal;2015-05
4. Numerical Simulation of Rotor-aerodynamic Surface Interaction in Hover Using Moving Chimera Grid;Chinese Journal of Aeronautics;2012-06
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