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NACA-RM-A51H02
Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds - plane triangular wing of aspect ratio 3 with NACA 0003-63 section
Year: 1951
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 design of high-speed fighter airplanes. The effects of variations in plan form, twist, camber, and thickness are being investigated. This report is one 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 3 and NACA 0003-63 sections in stream wise planes. Results of other investigations in this program are presented in references 1 to 10. As in these references, the data herein are presented without analysis to expedite publication.
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 design of high-speed fighter airplanes. The effects of variations in plan form, twist, camber, and thickness are being investigated. This report is one 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 3 and NACA 0003-63 sections in stream wise planes. Results of other investigations in this program are presented in references 1 to 10. As in these references, the data herein are presented without analysis to expedite publication.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:10:50Z | |
| date available | 2017-09-04T16:10:50Z | |
| date copyright | 01/01/1951 | |
| date issued | 1951 | |
| identifier other | SKMCWDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/74064 | |
| 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 design of high-speed fighter airplanes. The effects of variations in plan form, twist, camber, and thickness are being investigated. This report is one 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 3 and NACA 0003-63 sections in stream wise planes. Results of other investigations in this program are presented in references 1 to 10. As in these references, the data herein are presented without analysis to expedite publication. | |
| language | English | |
| title | NACA-RM-A51H02 | num |
| title | Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds - plane triangular wing of aspect ratio 3 with NACA 0003-63 section | en |
| type | standard | |
| page | 21 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1951 | |
| contenttype | fulltext |