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NASA-TN-D-4929
Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow
Year: 1968
Abstract: Computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in compressible flow
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:45:47Z | |
| date available | 2017-09-04T18:45:47Z | |
| date copyright | 01/01/1968 | |
| date issued | 1968 | |
| identifier other | KHYKAEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsessionid=3826AF679D40527318548F1EFDEC014A/handle/yse/227120 | |
| description abstract | Computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in compressible flow | |
| language | English | |
| title | NASA-TN-D-4929 | num |
| title | Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow | en |
| type | standard | |
| page | 79 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1968 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | ANGLE | |
| subject keywords | ATTACK | |
| subject keywords | COMPRESSIBILITY | |
| subject keywords | COMPRESSIBLE | |
| subject keywords | EFFECTS | |
| subject keywords | FLOW | |
| subject keywords | LOADING | |
| subject keywords | ROLL | |
| subject keywords | SIDESLIP | |
| subject keywords | SPAN | |
| subject keywords | STABILITY | |
| subject keywords | VORTICES | |
| subject keywords | WING | |
| subject keywords | YAW |