درباره ما
NACA-TN-2504
Effects of wing position and horizontal-tail position on the static stability characteristics of models with unswept and 45 degree sweptback surfaces with some reference to mutual interference
Year: 1951
Abstract: An investigation was made to determine the effects of wing position and horizontal-tail position on the low-speed static longitudinal and static lateral stability characteristics of airplane models having unswept and 45° sweptback surfaces.
Subject: AIRPLANES
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:23:34Z | |
| date available | 2017-09-04T15:23:34Z | |
| date copyright | 01/01/1951 | |
| date issued | 1951 | |
| identifier other | NFPTYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/23837 | |
| description abstract | An investigation was made to determine the effects of wing position and horizontal-tail position on the low-speed static longitudinal and static lateral stability characteristics of airplane models having unswept and 45° sweptback surfaces. | |
| language | English | |
| title | NACA-TN-2504 | num |
| title | Effects of wing position and horizontal-tail position on the static stability characteristics of models with unswept and 45 degree sweptback surfaces with some reference to mutual interference | en |
| type | standard | |
| page | 59 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1951 | |
| contenttype | fulltext | |
| subject keywords | AIRPLANES | |
| subject keywords | COMBINATIONS | |
| subject keywords | COMPLETE | |
| subject keywords | FUSELAGE | |
| subject keywords | STABILITY | |
| subject keywords | STATIC | |
| subject keywords | SWEEP | |
| subject keywords | TAIL | |
| subject keywords | WING | |
| subject keywords | WINGS |