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NASA-TN-D-8391
Calculations, and comparison with an ideal minimum, of trimmed drag for conventional and canard configurations having various levels of static stability
Year: 1977
Abstract: Classical drag equations were used to calculate total and induced drag and ratios of stabilizer lift to wing lift for a variety of conventional and canard configurations. The Flight efficiencies of such configurations that are trimmed in pitch and have various values of static margin are evaluated. Classical calculation methods are compared with more modern lifting surface theory.
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:51:36Z | |
| date available | 2017-09-04T16:51:36Z | |
| date copyright | 01/01/1977 | |
| date issued | 1977 | |
| identifier other | WQYKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/115193 | |
| description abstract | Classical drag equations were used to calculate total and induced drag and ratios of stabilizer lift to wing lift for a variety of conventional and canard configurations. The Flight efficiencies of such configurations that are trimmed in pitch and have various values of static margin are evaluated. Classical calculation methods are compared with more modern lifting surface theory. | |
| language | English | |
| title | NASA-TN-D-8391 | num |
| title | Calculations, and comparison with an ideal minimum, of trimmed drag for conventional and canard configurations having various levels of static stability | en |
| type | standard | |
| page | 25 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1977 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | AIRCRAFT | |
| subject keywords | CANARD | |
| subject keywords | CONFIGURATIONS | |
| subject keywords | DEVICES | |
| subject keywords | DRAG | |
| subject keywords | INDUCED | |
| subject keywords | LIFT | |
| subject keywords | MEASUREMENT | |
| subject keywords | RATIO | |
| subject keywords | STABILITY | |
| subject keywords | STATIC | |
| subject keywords | STRUCTURES | |
| subject keywords | TANDEM | |
| subject keywords | WING |