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NACA-TN-4404
Effects of propeller position and overlap on the slipstream deflection characteristics of a wing-propeller configuration equipped with a sliding and fowler flap
Year: 1958
Abstract: An investigation has been made in a static-test facility at the Langley Aeronautical Laboratory to determine some of the effects of propeller position and overlap on the slipstream deflection characteristics of a configuration equipped with a sliding and Fowler flap. The effects of a leading-edge slat, nacelle size, flap segmentation ,and number of propellers were also investigated. .
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:30:44Z | |
| date available | 2017-09-04T15:30:44Z | |
| date copyright | 01/01/1958 | |
| date issued | 1958 | |
| identifier other | OBOUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/32184 | |
| description abstract | An investigation has been made in a static-test facility at the Langley Aeronautical Laboratory to determine some of the effects of propeller position and overlap on the slipstream deflection characteristics of a configuration equipped with a sliding and Fowler flap. The effects of a leading-edge slat, nacelle size, flap segmentation ,and number of propellers were also investigated. . | |
| language | English | |
| title | NACA-TN-4404 | num |
| title | Effects of propeller position and overlap on the slipstream deflection characteristics of a wing-propeller configuration equipped with a sliding and fowler flap | en |
| type | standard | |
| page | 82 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1958 | |
| contenttype | fulltext |