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NACA-TR-540
Interference of wing and fuselage from tests of 209 combinations in the NACA variable-density tunnel
Year: 1936
Abstract: This report presents the results of tests of 209 simple wing-fuselage combinations made in the NACA variable-density wind tunnel to provide information regarding the effects of aerodynamic interference between wings and fuselages at a large value of Reynolds number.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:54:21Z | |
| date available | 2017-09-04T15:54:21Z | |
| date copyright | 01/01/1936 | |
| date issued | 1936 | |
| identifier other | QRWUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/57654 | |
| description abstract | This report presents the results of tests of 209 simple wing-fuselage combinations made in the NACA variable-density wind tunnel to provide information regarding the effects of aerodynamic interference between wings and fuselages at a large value of Reynolds number. | |
| language | English | |
| title | NACA-TR-540 | num |
| title | Interference of wing and fuselage from tests of 209 combinations in the NACA variable-density tunnel | en |
| type | standard | |
| page | 44 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1936 | |
| contenttype | fulltext |