What is it about?
Shrouded rotor perfomance at hovering condition changing shroud length, and bell mouse shape.
Featured Image
Read the Original
This page is a summary of: Evaluation of Hovering Thrust Performance of Shrouded Rotors for Multi-rotor UAVs to Reduce Weight, January 2015, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2015-0013.
You can read the full text:
Contributors
The following have contributed to this page
