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NACA-ACR-L4F23
Wind-tunnel investigation of control-surface characteristics XIX - a double flap with an overhang and an internal aerodynamic balance
Year: 1944
Abstract: Wind-tunnel tests have been made in two-dimensional flow to investigate the aerodynamic characteristics of a double flap with an internal and an overhang balance. Three sizes of each typee of balance were tested with three relative rates of deflection of the two flaps. An NAACA 66-009 airfoil having a 0.30-airfoil-chord straight-contour forward flap and.a 0.20-airfoil-chord straight-contour rearward flap was used.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:03:53Z | |
| date available | 2017-09-04T17:03:53Z | |
| date copyright | 01/01/1944 | |
| date issued | 1944 | |
| identifier other | XYDZYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho1626ear39D40206861598F1ED52F014A/handle/yse/127466 | |
| description abstract | Wind-tunnel tests have been made in two-dimensional flow to investigate the aerodynamic characteristics of a double flap with an internal and an overhang balance. Three sizes of each typee of balance were tested with three relative rates of deflection of the two flaps. An NAACA 66-009 airfoil having a 0.30-airfoil-chord straight-contour forward flap and.a 0.20-airfoil-chord straight-contour rearward flap was used. | |
| language | English | |
| title | NACA-ACR-L4F23 | num |
| title | Wind-tunnel investigation of control-surface characteristics XIX - a double flap with an overhang and an internal aerodynamic balance | en |
| type | standard | |
| page | 53 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1944 | |
| contenttype | fulltext |