A Study of Aerodynamic Characteristics of Airfoil in ground Effects using Rotating Disc
| Project/Area Number |
21560182
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| Research Category |
Grant-in-Aid for Scientific Research (C)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Fluid engineering
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| Research Institution | University of Miyazaki |
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Principal Investigator |
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| Project Period (FY) |
2009 – 2011
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| Project Status |
Completed (Fiscal Year 2011)
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| Budget Amount *help |
¥4,420,000 (Direct Cost: ¥3,400,000、Indirect Cost: ¥1,020,000)
Fiscal Year 2011: ¥910,000 (Direct Cost: ¥700,000、Indirect Cost: ¥210,000)
Fiscal Year 2010: ¥1,300,000 (Direct Cost: ¥1,000,000、Indirect Cost: ¥300,000)
Fiscal Year 2009: ¥2,210,000 (Direct Cost: ¥1,700,000、Indirect Cost: ¥510,000)
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| Keywords | 圧縮・非圧縮 / 翼 / 地面効果 / 圧縮・非圧縮性流れ / 交通システム |
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| Research Abstract |
When an airfoil moves close to a ground, it interferes strongly with the ground through the fluid viscosity. In order to reconstruct the circumstances the airfoil moves relative to the ground, the circulating disc apparatus was used. The aerodynamic characteristics ; lift, drag coefficients and the ground pressure distributions along the wing direction were measured. Numerical simulations of the fluid flows around the airfoil were also carried. After the numerical accuracy was confirmed, the details of the characteristics of the airfoil were clarified. Then, the aerodynamic characteristics of the three dimensional wing of AEROTRAIN in ground effects was elucidated.
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Report
(4 results)
Research Products
(7 results)
