درباره ما
NASA-TN-D-6091
Dynamic stability derivatives of a twin-jet fighter model for angles of attack from -10 degrees to 110 degrees
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:49:24Z | |
| date available | 2017-09-04T16:49:24Z | |
| date copyright | 01/01/1971 | |
| date issued | 1971 | |
| identifier other | WKYKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/112906 | |
| description abstract | Dynamic stability derivatives of twin-jet fighter model for angles of attack from -10 deg to 110 deg | |
| language | English | |
| title | NASA-TN-D-6091 | num |
| title | Dynamic stability derivatives of a twin-jet fighter model for angles of attack from -10 degrees to 110 degrees | en |
| type | standard | |
| page | 39 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1971 | |
| contenttype | fulltext | |
| subject keywords | AIRCRAFT | |
| subject keywords | ANGLE | |
| subject keywords | ATTACK | |
| subject keywords | DYNAMIC | |
| subject keywords | FIGHTER | |
| subject keywords | INCLINATION | |
| subject keywords | PITCH | |
| subject keywords | ROLL | |
| subject keywords | STABILITY | |
| subject keywords | SWEPT | |
| subject keywords | WINGS | |
| subject keywords | YAW |
