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NACA-TN-3904
Investigation of the effectiveness of boundary-layer control by blowing over a combination of sliding and plain flaps in deflecting a propeller slipstream downward for vertical take-off
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:11:22Z | |
| date available | 2017-09-04T18:11:22Z | |
| date copyright | 01/01/1956 | |
| date issued | 1956 | |
| identifier other | GZNUYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/194335 | |
| description abstract | An investigation was conducted in order to determine the effectiveness of blowing a jet of air over the flaps of a wing equipped with a 50-percent-chord sliding flap and a 25-percent-chord plain flap in deflecting a propeller slipstream downward for vertical take-off and the results are presented herein. The effects of a leading-edge slat, ground proximity, end plate, and propeller position were also investigated. The tests were conducted in a static-thrust facility at the Langley Aeronautical Laboratory. | |
| language | English | |
| title | NACA-TN-3904 | num |
| title | Investigation of the effectiveness of boundary-layer control by blowing over a combination of sliding and plain flaps in deflecting a propeller slipstream downward for vertical take-off | en |
| type | standard | |
| page | 45 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1956 | |
| contenttype | fulltext | |
| subject keywords | AIRPLANES | |
| subject keywords | COMPLETE | |
| subject keywords | DEVICES | |
| subject keywords | HIGH | |
| subject keywords | LIFT | |
| subject keywords | LONGITUDINAL | |
| subject keywords | PERFORMANCE | |
| subject keywords | PROPELLERS | |
| subject keywords | SLIPSTREAM | |
| subject keywords | STABILITY | |
| subject keywords | STATIC | |
| subject keywords | WINGS |
