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NACA-RM-L7E13
Effects of a Fuselage on the Aerodynamic Characteristics of a 42 Degrees Sweptback Wing at Reynolds Numbers to 8,000,000
Year: 1947
Abstract: Wind-tunnel investigations were made in pitch and yaw with and without split flaps. Presence of the fuselage had negligible effect on values of maximum lift coefficient and slope of lift curve, but caused a destabilizing shift in the rate of change of pitching moment with lift. Effects of fuselage position on drag characteristics were small for wings without flaps, but were appreciable when split flaps were on.
Subject: FLAPPING
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:00:48Z | |
| date available | 2017-09-04T16:00:48Z | |
| date copyright | 17446 | |
| date issued | 1947 | |
| identifier other | RJMCWDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/64011 | |
| description abstract | Wind-tunnel investigations were made in pitch and yaw with and without split flaps. Presence of the fuselage had negligible effect on values of maximum lift coefficient and slope of lift curve, but caused a destabilizing shift in the rate of change of pitching moment with lift. Effects of fuselage position on drag characteristics were small for wings without flaps, but were appreciable when split flaps were on. | |
| language | English | |
| title | NACA-RM-L7E13 | num |
| title | Effects of a Fuselage on the Aerodynamic Characteristics of a 42 Degrees Sweptback Wing at Reynolds Numbers to 8,000,000 | en |
| type | standard | |
| page | 34 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1947 | |
| contenttype | fulltext | |
| subject keywords | FLAPPING | |
| subject keywords | FLAPS | |
| subject keywords | FUSELAGES | |
| subject keywords | SPLIT | |
| subject keywords | WINGS |