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NACA-TR-1056
Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds
Year: 1951
Abstract: A simplified lifting-surface theory that includes effects of compressibility and spanwise variation of section lift-curve slope is used to provide charts with which antisymmetric loading due to arbitrary antisymmetric angle of attack can be found for wings having symmetric plan forms with a constant spanwise sweep angle of the quarter-chord line. Consideration is given to the flexible wing in roll. Aerodynamic characteristics due to rolling, deflected ailerons, and sideslip of wings with dihedral are considered. Solutions are presented for straight-tapered wings for a range of swept plan forms.
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:56:11Z | |
| date available | 2017-09-04T15:56:11Z | |
| date copyright | 01/01/1951 | |
| date issued | 1951 | |
| identifier other | QXDZYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/59535 | |
| description abstract | A simplified lifting-surface theory that includes effects of compressibility and spanwise variation of section lift-curve slope is used to provide charts with which antisymmetric loading due to arbitrary antisymmetric angle of attack can be found for wings having symmetric plan forms with a constant spanwise sweep angle of the quarter-chord line. Consideration is given to the flexible wing in roll. Aerodynamic characteristics due to rolling, deflected ailerons, and sideslip of wings with dihedral are considered. Solutions are presented for straight-tapered wings for a range of swept plan forms. | |
| language | English | |
| title | NACA-TR-1056 | num |
| title | Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds | en |
| type | standard | |
| page | 40 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1951 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | AILERONS | |
| subject keywords | ANTISYMMETRY | |
| subject keywords | BODIES | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | COMPRESSIBILITY | |
| subject keywords | COMPUTATIONAL | |
| subject keywords | DEFLECTION | |
| subject keywords | DYNAMICS | |
| subject keywords | EFFECTS | |
| subject keywords | FLOW | |
| subject keywords | FLUID | |
| subject keywords | LOADING | |
| subject keywords | LOADS | |
| subject keywords | PLANFORMS | |
| subject keywords | ROLL | |
| subject keywords | SIDESLIP | |
| subject keywords | SPAN | |
| subject keywords | SUBSONIC | |
| subject keywords | SWEPT | |
| subject keywords | SYMMETRICAL | |
| subject keywords | WING | |
| subject keywords | WINGS |