On the Effects of an Installed Propeller Slipstream on Wing Aerodynamic Characteristics

This work presents an experimental study of the effect of an installed propeller slipstream on a wing boundary layer. The main objective was to analyse through wind tunnel experiments the effect of the propeller slipstream on the wing boundary layer characteristics such as: laminar flow extension an...

詳細記述

書誌詳細
出版年:Acta Polytechnica
第一著者: F. M. Catalano
フォーマット: 論文
言語:英語
出版事項: CTU Central Library 2004-01-01
主題:
オンライン・アクセス:https://ojs.cvut.cz/ojs/index.php/ap/article/view/562