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NASA-TN-D-3159
Aerodynamic damping and oscillatory stability in pitch for a model of a typical subsonic jet-transport airplane
Year: 1966
Abstract: Aerodynamic damping and oscillatory stability in pitch for model of typical swept wing subsonic jet transport
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:49:39Z | |
| date available | 2017-09-04T17:49:39Z | |
| date copyright | 01/01/1966 | |
| date issued | 1966 | |
| identifier other | EUTKAEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/172948 | |
| description abstract | Aerodynamic damping and oscillatory stability in pitch for model of typical swept wing subsonic jet transport | |
| language | English | |
| title | NASA-TN-D-3159 | num |
| title | Aerodynamic damping and oscillatory stability in pitch for a model of a typical subsonic jet-transport airplane | en |
| type | standard | |
| page | 17 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1966 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | AIRCRAFT | |
| subject keywords | CONTROL | |
| subject keywords | DAMPING | |
| subject keywords | FLOW | |
| subject keywords | GAS | |
| subject keywords | JET | |
| subject keywords | JETS | |
| subject keywords | LONGITUDINAL | |
| subject keywords | MACH | |
| subject keywords | NUMBER | |
| subject keywords | OSCILLATIONS | |
| subject keywords | PITCH | |
| subject keywords | REYNOLDS | |
| subject keywords | STABILITY | |
| subject keywords | SUBSONIC | |
| subject keywords | SWEPT | |
| subject keywords | TRANSPORT | |
| subject keywords | WING | |
| subject keywords | WINGS |