Euler calculations for flowfield of a helicopter rotor in hover
- 1 April 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 24 (4) , 231-238
- https://doi.org/10.2514/3.45431
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- A Three-Dimensional Euler Solver for Turbomachinery Blade RowsJournal of Engineering for Gas Turbines and Power, 1985
- Subsonic and Transonic Potential Flow over Helicopter Rotor BladesAIAA Journal, 1972