A method for modeling finite-core vortices in wake-flow calculations
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1984-417
Reference37 articles.
1. The Wake Geometry of a Hovering Helicopter Rotor and Its Influence on Rotor Performance
2. Navier-Stokes calculations for the vortex wake of a rotor in hover
3. Vortex methods for flow simulation
Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Numerical study of sound generation due to a spinning vortex pair;AIAA Journal;1995-01
2. Calculation of flow about two-dimensional bodies by means of the velocity-vorticity formulation on a staggered grid;29th Aerospace Sciences Meeting;1991-01-07
3. Nonlinear aerodynamics of two-dimensional airfoils in severe maneuver;AIAA Journal;1990-03
4. Simulation of realistic rotor blade-vortex interactions using a finite-difference technique;20th Fluid Dynamics, Plasma Dynamics and Lasers Conference;1989-06-12
5. Unsteady wing theory - The Karman/Sears legacy;1st National Fluid Dynamics Conference;1988-07-25
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