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NACA-ARR-L4J05
Wind-tunnel investigation of an NACA 23021 airfoil with a 0.32-airfoil-chord double slotted flap
Year: 1944
Abstract: An investigation was made in the LML 7- by 10-foot wind tunnel of an NACA 23021 airfoil with a double slotted flap having a chord 32 percent of the airfoil chord (0.32c) to determine the aerodynamic section characteristics with the flaps deflected at various positions. The effects of moving the fore flap and rear flap as a unit and of deflecting or removing the lower lap of the slot were also determined.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:14:21Z | |
| date available | 2017-09-04T16:14:21Z | |
| date copyright | 01/01/1944 | |
| date issued | 1944 | |
| identifier other | STUYYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/77571 | |
| description abstract | An investigation was made in the LML 7- by 10-foot wind tunnel of an NACA 23021 airfoil with a double slotted flap having a chord 32 percent of the airfoil chord (0.32c) to determine the aerodynamic section characteristics with the flaps deflected at various positions. The effects of moving the fore flap and rear flap as a unit and of deflecting or removing the lower lap of the slot were also determined. | |
| language | English | |
| title | NACA-ARR-L4J05 | num |
| title | Wind-tunnel investigation of an NACA 23021 airfoil with a 0.32-airfoil-chord double slotted flap | en |
| type | standard | |
| page | 54 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1944 | |
| contenttype | fulltext |