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NASA-TN-D-6440
Dynamic stability derivatives of a jet transport configuration with high thrust-weight ratio and an externally blown jet flap
Year: 1971
Abstract: Dynamic stability of jet transport configuration with high thrust-weight ratio and externally blown jet flap
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:10:39Z | |
| date available | 2017-09-04T16:10:39Z | |
| date copyright | 01/01/1971 | |
| date issued | 1971 | |
| identifier other | SJYKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/73891 | |
| description abstract | Dynamic stability of jet transport configuration with high thrust-weight ratio and externally blown jet flap | |
| language | English | |
| title | NASA-TN-D-6440 | num |
| title | Dynamic stability derivatives of a jet transport configuration with high thrust-weight ratio and an externally blown jet flap | en |
| type | standard | |
| page | 84 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1971 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | AIRCRAFT | |
| subject keywords | ANGLE | |
| subject keywords | ATTACK | |
| subject keywords | CONFIGURATIONS | |
| subject keywords | ENGINES | |
| subject keywords | FLAPS | |
| subject keywords | JET | |
| subject keywords | MODELS | |
| subject keywords | RATIO | |
| subject keywords | STABILITY | |
| subject keywords | THRUST | |
| subject keywords | TRANSPORT | |
| subject keywords | TURBOFAN | |
| subject keywords | WEIGHT |