NACA-TN-3963
A correlation of low-speed, airfoil-section stalling characteristics with Reynolds number and airfoil geometry
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:45:25Z | |
| date available | 2017-09-04T16:45:25Z | |
| date copyright | 01/01/1957 | |
| date issued | 1957 | |
| identifier other | VZNUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/108708 | |
| description abstract | The low-speed stalling characteristics of a large number of airfoil sections have been correlated with Reynolds number and a single airfoil ordinate near the leading edge as the correlating parameters. The correlation is appropriate only to airfoils without high-lift devices in flows of very low turbulence and with aerodynamically smooth surfaces. | |
| language | English | |
| title | NACA-TN-3963 | num |
| title | A correlation of low-speed, airfoil-section stalling characteristics with Reynolds number and airfoil geometry | en |
| type | standard | |
| page | 10 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1957 | |
| contenttype | fulltext |

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