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NACA-WR-L-511
Wind-tunnel investigation of control-surface characteristics XII - various cover-plate alinements on the NACA 0015 airfoil with a 30-percent-chord flap and large sealed internal balance
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:05:38Z | |
| date available | 2017-09-04T18:05:38Z | |
| date copyright | 01/01/1943 | |
| date issued | 1943 | |
| identifier other | GJZYYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/188513 | |
| description abstract | Force-test measurements in two-dimensional flow have been made in the NACA 4- by 6-foot vertical tunnel to determine the aerodynamic effects of changing the alinement of the cover plates on a sealed internally balanced flap. An NACA 0015 airfoil was utilized for the tests. The chord of the straight-contour flap was 30 percent of the airfoil chord and the balance was 50 percent of the flap chord. | |
| language | English | |
| title | NACA-WR-L-511 | num |
| title | Wind-tunnel investigation of control-surface characteristics XII - various cover-plate alinements on the NACA 0015 airfoil with a 30-percent-chord flap and large sealed internal balance | en |
| type | standard | |
| page | 27 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1943 | |
| contenttype | fulltext |
