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NACA-TN-2010
Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces
Year: 1950
Abstract: An investigation has been conducted in the Langley stability tunnel to determine the effects of changes in horizontal-tail size and location on the static lateral stability characteristics of a complete model with wing and tail surfaces having the quarter-chord line swept back 45º.
Available procedures, based on analyses of unswept-tail configurations, for predicting the effect of the horizontal tail on directional stability, were found to be unreliable when applied to swept-tail configurations.
Available procedures, based on analyses of unswept-tail configurations, for predicting the effect of the horizontal tail on directional stability, were found to be unreliable when applied to swept-tail configurations.
Subject: AIRFOILS
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:07:52Z | |
| date available | 2017-09-04T17:07:52Z | |
| date copyright | 01/01/1950 | |
| date issued | 1950 | |
| identifier other | YJAUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/131449 | |
| description abstract | An investigation has been conducted in the Langley stability tunnel to determine the effects of changes in horizontal-tail size and location on the static lateral stability characteristics of a complete model with wing and tail surfaces having the quarter-chord line swept back 45º. Available procedures, based on analyses of unswept-tail configurations, for predicting the effect of the horizontal tail on directional stability, were found to be unreliable when applied to swept-tail configurations. | |
| language | English | |
| title | NACA-TN-2010 | num |
| title | Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces | en |
| type | standard | |
| page | 47 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1950 | |
| contenttype | fulltext | |
| subject keywords | AIRFOILS | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | COMBINATIONS | |
| subject keywords | DRAG | |
| subject keywords | FUSELAGE | |
| subject keywords | HORIZONTAL | |
| subject keywords | LATERAL | |
| subject keywords | LOW | |
| subject keywords | NACA | |
| subject keywords | ORDINATES | |
| subject keywords | POSITION | |
| subject keywords | STABILITY | |
| subject keywords | STATIC | |
| subject keywords | SURFACES | |
| subject keywords | SWEPTBACK | |
| subject keywords | TAIL | |
| subject keywords | TESTS | |
| subject keywords | TUNNEL | |
| subject keywords | WIND | |
| subject keywords | WING | |
| subject keywords | WINGS |