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NACA-RM-A53C19
Experimental investigation of the effects of plan-form taper on the aerodynamic characteristics of symmetrical unswept wings of varying aspect ratio
Year: 1953
Abstract: INTRODUCTION
A great number of data axe available on the aerodynamic characteristics of tapered wings at high subsonic speeds; however these data cu?e difficult to correlate because of the differences in testing,techniques used. It is the purpose of this investigation to provide comprehensive data on the effects of plan-form taper on the aerodynamic characteristics of a family of symmetrical, unswept wings.
Nine wings, in all} were investigated, three aspect ratio 4 wings having taper ratios of 1.00s 0.502 and 0.20; three aspect ratio 3 wings having taper ratios of 1.00, 0.60, and 0.33; and three aspect ratio 2 . wings having taper ratios of 1.00,0.71, and 0.50. The profiles of all wings were the NACA 63A008. The wings were tested in combination with four different bodies of revolution to help differentiate between the effects of taper and wing-body interference.
A great number of data axe available on the aerodynamic characteristics of tapered wings at high subsonic speeds; however these data cu?e difficult to correlate because of the differences in testing,techniques used. It is the purpose of this investigation to provide comprehensive data on the effects of plan-form taper on the aerodynamic characteristics of a family of symmetrical, unswept wings.
Nine wings, in all} were investigated, three aspect ratio 4 wings having taper ratios of 1.00s 0.502 and 0.20; three aspect ratio 3 wings having taper ratios of 1.00, 0.60, and 0.33; and three aspect ratio 2 . wings having taper ratios of 1.00,0.71, and 0.50. The profiles of all wings were the NACA 63A008. The wings were tested in combination with four different bodies of revolution to help differentiate between the effects of taper and wing-body interference.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:16:17Z | |
| date available | 2017-09-04T17:16:17Z | |
| date copyright | 01/01/1953 | |
| date issued | 1953 | |
| identifier other | ZFMCWDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/139726 | |
| description abstract | INTRODUCTION A great number of data axe available on the aerodynamic characteristics of tapered wings at high subsonic speeds; however these data cu?e difficult to correlate because of the differences in testing,techniques used. It is the purpose of this investigation to provide comprehensive data on the effects of plan-form taper on the aerodynamic characteristics of a family of symmetrical, unswept wings. Nine wings, in all} were investigated, three aspect ratio 4 wings having taper ratios of 1.00s 0.502 and 0.20; three aspect ratio 3 wings having taper ratios of 1.00, 0.60, and 0.33; and three aspect ratio 2 . wings having taper ratios of 1.00,0.71, and 0.50. The profiles of all wings were the NACA 63A008. The wings were tested in combination with four different bodies of revolution to help differentiate between the effects of taper and wing-body interference. | |
| language | English | |
| title | NACA-RM-A53C19 | num |
| title | Experimental investigation of the effects of plan-form taper on the aerodynamic characteristics of symmetrical unswept wings of varying aspect ratio | en |
| type | standard | |
| page | 55 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1953 | |
| contenttype | fulltext |