Solution method for a hovering helicopter rotor using the Euler equations
Authors:
- 14 January 1985
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Computation of flow around wings based on the Euler equationsJournal of Fluid Mechanics, 1984
- A computational method for helicopter vortex wakes1984
- Computation of simple three-dimensional wing-vortex interaction in transonic flow1981
- Implicit Finite-Difference Procedures for the Computation of Vortex WakesAIAA Journal, 1977
- Subsonic and Transonic Potential Flow over Helicopter Rotor BladesAIAA Journal, 1972