درباره ما
NACA-TN-3857
Experimental investigation at low speed of the effects of wing position on the static stability of models having fuselages of various cross section and unswept and 45 degrees sweptback surfaces
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:38:47Z | |
| date available | 2017-09-04T15:38:47Z | |
| date copyright | 01/01/1956 | |
| date issued | 1956 | |
| identifier other | AZNUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/40879 | |
| description abstract | An experimental investigation was made to determine the effects of wing position on the low-speed static longitudinal and static lateral stability derivatives of airplane models having fuselages of square and rectangular cross sections and unswept and 45° sweptback surfaces. The horizontal tail of each model was located on the fuselage center line. | |
| language | English | |
| title | NACA-TN-3857 | num |
| title | Experimental investigation at low speed of the effects of wing position on the static stability of models having fuselages of various cross section and unswept and 45 degrees sweptback surfaces | en |
| type | standard | |
| page | 78 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1956 | |
| contenttype | fulltext |
