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NACA-ACR-L5F27
Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(sub 1)-210 airfoil section
Year: 1945
Abstract: An investigation was made of three interchangeable sealed-gap 0.20-airfoil –chord plain ailerons of different contour on the NACA 65-210 airfoil section. The three aileron contours tested were the true airfoil contour, straight sides, and a beveled trailing edge. The effects of aileron contour on the section aerodynamic characteristics of the airfoil and aileron are presented herein.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:55:18Z | |
| date available | 2017-09-04T15:55:18Z | |
| date copyright | 01/01/1945 | |
| date issued | 1945 | |
| identifier other | QUUYYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho47037D83FCDCAC426159DD6E273C9FCD/handle/yse/58694 | |
| description abstract | An investigation was made of three interchangeable sealed-gap 0.20-airfoil –chord plain ailerons of different contour on the NACA 65-210 airfoil section. The three aileron contours tested were the true airfoil contour, straight sides, and a beveled trailing edge. The effects of aileron contour on the section aerodynamic characteristics of the airfoil and aileron are presented herein. | |
| language | English | |
| title | NACA-ACR-L5F27 | num |
| title | Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(sub 1)-210 airfoil section | en |
| type | standard | |
| page | 59 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1945 | |
| contenttype | fulltext |