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title低Re 数領域におけるNACA0012翼面上の圧力分布
Other TitlePressure Distribution on a NACA0012 Airfoil at Low Reynolds Numbers
Author(jpn)山口裕太; 大竹, 智久; 村松, 旦典
Author(eng)Yamaguchi, Yuta; Ohtake, Tomohisa; Muramatsu, Akinori
Author Affiliation(jpn)日本大学大学院; 日本大学理工学部; 日本大学理工学部
Author Affiliation(eng)Graduate School, Nihon University; College of Science and Technology, Nihon University; College of Science and Technology, Nihon University
Issue Date2014-03-31
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構特別資料: 第45回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2013論文集
JAXA Special Publication
Start page127
End page130
Publication date2014-03-31
AbstractThe pressure distribution on a NACA0012 airfoil was measured in order to clarify the flow field around the airfoil in the low-Reynolds-number region from 10,000 to 50,000. In the present study, a wind tunnel and a NACA0012 wing model with 70 static pressure ports were used for the measurements. The pressure on the airfoil surface was measured by a micro-pressure sensor. Based on the obtained pressure distributions, we confirmed in detail the behavior of the separation bubble and observed the change of a short bubble into a long bubble. As the angle of attack was increased, the non-linearity of the aerodynamic characteristics was affected by both changes in the separation point and the length of the separation bubble. We confirmed that the behavior of the separation bubble is affected by flow field phenomena that depend on the Reynolds number.
Description会議情報: 第45回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2013 (2013年7月4日-5日. タワーホール船堀), 東京
形態: カラー図版あり
Meeting Information: 45th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2013 (July 4-5, 2013. Tower Hall Funabori), Tokyo, Japan
Physical characteristics: Original contains color illustrations
Document TypeConference Paper
JAXA Category特別資料
NASA Subject CategoryResearch and Support Facilities (Air)
Report NoJAXA-SP-13-011

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