Effect of Multiple Grooves on Aerodynamic Performance of a Low Reynolds Number UAV Propeller (Part II)

In an continuation of work previously performed by the author on grooved propellers, numerical investigations are performed on Applied Precision Composites 10×7 Slow Flyer propeller. Computational Fluid Dynamics is used to analyze the novel design. The grooved sections considered have a rectangular...

詳細記述

書誌詳細
出版年:INCAS Bulletin
第一著者: Aravind SEENI
フォーマット: 論文
言語:英語
出版事項: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2023-06-01
主題:
オンライン・アクセス:https://bulletin.incas.ro/files/seeni__vol_15_iss_2__a_2.pdf