Efficient method for calculating the axial velocities induced along rotating blades by trailing helical vortices
- 1 June 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 21 (6) , 433-435
- https://doi.org/10.2514/3.44984
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- ON THE EFFECTS OF SCALE AND ROUGHNESS ON FREE RUNNING PROPELLERSJournal of the American Society for Naval Engineers, 1951