درباره ما
NACA-TR-460
The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel
Year: 1933
Abstract: An investigation of a large group of related airfoils was made in the NACA variable-density wind tunnel at a large value of the Reynolds number. The tests were made to provide data that may be directly employed for a rational choice of the most suitable airfoil section for a given application. The variation of the aerodynamic characteristics with variations in thickness and mean-line form were systematically studied. (author)
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:27:04Z | |
| date available | 2017-09-04T16:27:04Z | |
| date copyright | 01/01/1933 | |
| date issued | 1933 | |
| identifier other | UBXUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/90222 | |
| description abstract | An investigation of a large group of related airfoils was made in the NACA variable-density wind tunnel at a large value of the Reynolds number. The tests were made to provide data that may be directly employed for a rational choice of the most suitable airfoil section for a given application. The variation of the aerodynamic characteristics with variations in thickness and mean-line form were systematically studied. (author) | |
| language | English | |
| title | NACA-TR-460 | num |
| title | The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel | en |
| type | standard | |
| page | 61 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1933 | |
| contenttype | fulltext |