درباره ما
NASA-TN-D-5102
Large-scale tests of an airplane model with a double-delta wing, including longitudinal and lateral characteristics and ground effects
Year: 1969
Abstract: Aerodynamic characteristics and ground effects of supersonic transport with double delta wing
Subject: AERODYNAMIC
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:19:20Z | |
| date available | 2017-09-04T16:19:20Z | |
| date copyright | 01/01/1969 | |
| date issued | 1969 | |
| identifier other | THYKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/82804 | |
| description abstract | Aerodynamic characteristics and ground effects of supersonic transport with double delta wing | |
| language | English | |
| title | NASA-TN-D-5102 | num |
| title | Large-scale tests of an airplane model with a double-delta wing, including longitudinal and lateral characteristics and ground effects | en |
| type | standard | |
| page | 83 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1969 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | AERODYNAMICS | |
| subject keywords | ANGLE | |
| subject keywords | ATTACK | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | DELTA | |
| subject keywords | DRAG | |
| subject keywords | EFFECT | |
| subject keywords | GROUND | |
| subject keywords | LIFT | |
| subject keywords | MODELS | |
| subject keywords | RATIO | |
| subject keywords | STABILITY | |
| subject keywords | SUPERSONIC | |
| subject keywords | TESTS | |
| subject keywords | TRANSPORTS | |
| subject keywords | TUNNEL | |
| subject keywords | WIND | |
| subject keywords | WINGS |