درباره ما
NACA-RM-A54J20
Effect of taper ratio on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 with 53.1 degrees sweepback of leading edge at subsonic and supersonic speeds
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:38:06Z | |
| date available | 2017-09-04T16:38:06Z | |
| date copyright | 01/01/1955 | |
| date issued | 1955 | |
| identifier other | VHMCWDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/101681 | |
| description abstract | INTRODUCTION As part of the continuing investigation of low-aspect-ratio wings by the NACA, the effects of taper ratio on the aerodynamic characteristics of swept wings of aspect ratio 3 at subsonic and supersonic speeds have been investigated in the Ames 6- by 6-foot supersonic wind tunnel. This report is devoted to the presentation and discussion of the results obtained during this study. | |
| language | English | |
| title | NACA-RM-A54J20 | num |
| title | Effect of taper ratio on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 with 53.1 degrees sweepback of leading edge at subsonic and supersonic speeds | en |
| type | standard | |
| page | 26 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1955 | |
| contenttype | fulltext |
