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NACA-WR-L-454
Wind-tunnel investigation of control-surface characteristics VI - a 30-percent-chord plain flap on the NACA 0015 airfoil
Year: 1942
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 equipped with a plain flap having a chord 30 percent of the airfoil chord and a plain tab having a chord 20 percent of the flap chord. The results are presented in the form of aerodynamic section characteristics for several flap and tab deflections and for a sealed and an unsealed gap at the flap nose.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:03:06Z | |
| date available | 2017-09-04T17:03:06Z | |
| date copyright | 01/01/1942 | |
| date issued | 1942 | |
| identifier other | BXXYYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/126691 | |
| 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 equipped with a plain flap having a chord 30 percent of the airfoil chord and a plain tab having a chord 20 percent of the flap chord. The results are presented in the form of aerodynamic section characteristics for several flap and tab deflections and for a sealed and an unsealed gap at the flap nose. | |
| language | English | |
| title | NACA-WR-L-454 | num |
| title | Wind-tunnel investigation of control-surface characteristics VI - a 30-percent-chord plain flap on the NACA 0015 airfoil | en |
| type | standard | |
| page | 24 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1942 | |
| contenttype | fulltext |