Efficient High-Resolution Wake Modeling Using the Vorticity Transport Equation
- 1 July 2005
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 43 (7), 1434-1443
- https://doi.org/10.2514/1.13679
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Modelling Rotor Wakes in Ground EffectJournal of the American Helicopter Society, 2004
- Modeling the Mutual Distortions of Interacting Helicopter and Aircraft WakesJournal of Aircraft, 2003
- A Particle Method and Adaptive Treecode for Vortex Sheet Motion in Three-Dimensional FlowJournal of Computational Physics, 2001
- Comparison of Induced Velocity Models for Helicopter Flight MechanicsJournal of Aircraft, 2000
- Developments and challenges in rotorcraft aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- Rotor Wake Modeling for Flight Dynamic Simulation of HelicoptersAIAA Journal, 2000
- A fast algorithm for particle simulationsJournal of Computational Physics, 1987
- A direct method for the solution of poisson's equation with neumann boundary conditions on a staggered grid of arbitrary sizeJournal of Computational Physics, 1976
- Articulated Rotor Blade Flapping Motion at Low Advance RatioJournal of the American Helicopter Society, 1972