Vortex theory for hovering rotors
Author:
- 1 December 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 20 (12) , 1754-1756
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Effect of Tip Shape on Blade Loading Characteristics and Wake Geometry for a Two‐Bladed Rotor in HoverJournal of the American Helicopter Society, 1980