درباره ما
NACA-TN-4397
Static longitudinal and lateral stability characteristics at low speed of 60 degrees sweptback-midwing models having wings with an aspect ratio of 2, 4, or 6
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:05:17Z | |
| date available | 2017-09-04T15:05:17Z | |
| date copyright | 01/01/1958 | |
| date issued | 1958 | |
| identifier other | LBOUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/2739 | |
| description abstract | A systematic investigation was performed in the Langley stability tunnel to determine the static longitudinal and lateral stability characteristics at low speed of a series of 60° sweptback-midwing models having wings with an aspect ratio of 2, 4, or 6. Although both static longitudinal and lateral stability data are presented, emphasis has been placed on the contribution of the various components and combinations of components to directional stability at high angels of attack. Also included are some comparisons with the directional stability characteristic of similar unswept-and 45°sweptback-wing cofiugurations. | |
| language | English | |
| title | NACA-TN-4397 | num |
| title | Static longitudinal and lateral stability characteristics at low speed of 60 degrees sweptback-midwing models having wings with an aspect ratio of 2, 4, or 6 | en |
| type | standard | |
| page | 42 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1958 | |
| contenttype | fulltext |
