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NACA-RM-L51A23
Flight determination of the effects of wing vortex generators of the aerodynamic characteristics of the Douglas D-558-I airplane
Year: 1951
Abstract: Tests were made of the Douglas D-558-1 airplane to determine the effect of wing vortex generators on some of the typical undesirable handling characteristics such as buffeting, lateral unsteadiness, change in trim, and loss in control effectiveness which have occurred on present-day aircraft flying at supercritical speeds. An arbitrary size, shape, and location of the generators were selected and the investigation was initiated to determine what benefits might be derived from the installation and whether further investigations would be warranted.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:01:31Z | |
| date available | 2017-09-04T17:01:31Z | |
| date copyright | 01/01/1951 | |
| date issued | 1951 | |
| identifier other | XRONEEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/125010 | |
| description abstract | Tests were made of the Douglas D-558-1 airplane to determine the effect of wing vortex generators on some of the typical undesirable handling characteristics such as buffeting, lateral unsteadiness, change in trim, and loss in control effectiveness which have occurred on present-day aircraft flying at supercritical speeds. An arbitrary size, shape, and location of the generators were selected and the investigation was initiated to determine what benefits might be derived from the installation and whether further investigations would be warranted. | |
| language | English | |
| title | NACA-RM-L51A23 | num |
| title | Flight determination of the effects of wing vortex generators of the aerodynamic characteristics of the Douglas D-558-I airplane | en |
| type | standard | |
| page | 24 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1951 | |
| contenttype | fulltext |