درباره ما
NACA-TN-3961
Effect of fuselage nose length and a canopy on the static longitudinal and lateral stability characteristics of 45 degrees sweptback airplane models having fuselages with square cross sections
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:16:19Z | |
| date available | 2017-09-04T16:16:19Z | |
| date copyright | 01/01/1957 | |
| date issued | 1957 | |
| identifier other | SZNUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/79629 | |
| description abstract | A find-tunnel investigation was made at low speed in the Langley stability tunnel to determine the effects of fuselage nose length (the fuselage fineness ratio varied from 7.4.1to 10.18) and a canopy on the static longitudinal and lateral stability characteristics of a complete model having a fuselage with square cross sections, a 45° sweptback wing of aspect ratio 3 mounted low on the fuselage, and a 45° sweptback horizontal tail of aspect ratio 4 mounted slightly above the wing chord plane. The data were obtained through an angle-of-attack range of -100 to 32° and an angle-of-sideslip ranges of -24° to 24° | |
| language | English | |
| title | NACA-TN-3961 | num |
| title | Effect of fuselage nose length and a canopy on the static longitudinal and lateral stability characteristics of 45 degrees sweptback airplane models having fuselages with square cross sections | en |
| type | standard | |
| page | 48 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1957 | |
| contenttype | fulltext |
