درباره ما
NACA-TR-791
A theoretical investigation of longitudinal stability of airplane with free controls including effect of friction in control system
Year: 1944
Abstract: The relation between the elevator hinge-moment parameters and the control-forces for changes in forward speed and in maneuvers is shown for several values of static stability and elevator mass balance.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:54:12Z | |
| date available | 2017-09-04T16:54:12Z | |
| date copyright | 01/01/1944 | |
| date issued | 1944 | |
| identifier other | WXWUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/117672 | |
| description abstract | The relation between the elevator hinge-moment parameters and the control-forces for changes in forward speed and in maneuvers is shown for several values of static stability and elevator mass balance. | |
| language | English | |
| title | NACA-TR-791 | num |
| title | A theoretical investigation of longitudinal stability of airplane with free controls including effect of friction in control system | en |
| type | standard | |
| page | 21 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1944 | |
| contenttype | fulltext |