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NACA-WR-L-448
Wind-tunnel investigation of control-surface characteristics VII - a medium aerodynamic balance of two nose shapes used with a 30-percent-chord flap on an NACA 0015 airfoil
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:11:12Z | |
| date available | 2017-09-04T18:11:12Z | |
| date copyright | 01/01/1942 | |
| date issued | 1942 | |
| identifier other | GZDZYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/194200 | |
| description abstract | Force-test measurements in two-dimensional flow have been made in the NACA 4- by 6-foot vertical tunnel of the characteristics of an NACA 0015 airfoil with a balanced flap having a chord 30 percent of the airfoil chord and a flap-nose overhang 35 percent of the flap chord. The effect on the aerodynamic section characteristics of the shape of the flap-nose overhang and the gap at the flap nose was investigated. A few tests were made to determine the effectiveness of a 20-percent-flap-chord tab on the balanced control surface. | |
| language | English | |
| title | NACA-WR-L-448 | num |
| title | Wind-tunnel investigation of control-surface characteristics VII - a medium aerodynamic balance of two nose shapes used with a 30-percent-chord flap on an NACA 0015 airfoil | en |
| type | standard | |
| page | 25 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1942 | |
| contenttype | fulltext |
