درباره ما
NACA-RM-A50K20
Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds - plane triangular wing of aspect ratio 2 with NACA 0008-63 section
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:48:50Z | |
| date available | 2017-09-04T17:48:50Z | |
| date copyright | 01/01/1951 | |
| date issued | 1951 | |
| identifier other | ESCTUDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/171986 | |
| description abstract | INTRODUCTION A research program is in progress at the Ames Aeronautical Laboratory to ascertain experimentally at subsonic and supersonic Mach numbers the characteristics of wings of interest in the deem of high-speed fighter airplanes. Variations in plan form, twist, camber, and thickness are being investigated. This report is the first of a series pertaining to this program and presents results of tests of a wing–body combination having a plane triangular wing of aspect ratio 2 and NACA 0008-63 sections in streamwise planes. To expedite publication, these data are presented herein without analysis. | |
| language | English | |
| title | NACA-RM-A50K20 | num |
| title | Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds - plane triangular wing of aspect ratio 2 with NACA 0008-63 section | en |
| type | standard | |
| page | 24 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1951 | |
| contenttype | fulltext |
