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ArticleJ-GLOBAL ID:200902212456634876整理番号:09A0737263

超小型飛行機のレイノルズ数領域における4%キャンバー翼型およびNACA0012翼型の空力特性

Aerodynamic Characteristics of 4% Cambered-Plate and NACA0012 Airfoil at the Reynolds Numbers Region for Micro Air Vehicles

著者:手塚亜聖(早稲田大学理工学術院基幹理工学部機械科学・航空学科)、砂田保人(東京大学大学院工学系研究科航空宇宙工学専攻)、李家賢一(東京大学大学院工学系研究科航空宇宙工学専攻)
資料名:日本航空宇宙学会論文集 巻:57 号:665 ページ:258-265 (J-STAGE)
発行年:2009年
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