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NACA-RM-L8I03
The effects of high-lift devices on the low-speed stability characteristics of a tapered 37.5 degree sweptback wing of aspect ratio 3 in straight and rolling flow
Year: 1948
Abstract: Contains results of tunnel tests to determine effects of various combinations of split flaps, slats, and nose slats on the stability characteristics of a tapered 37.5 degree sweptback wing of aspect ratio 3 in straight and rolling flow.
Subject: COMPLETE
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:47:50Z | |
| date available | 2017-09-04T16:47:50Z | |
| date copyright | 01/01/1948 | |
| date issued | 1948 | |
| identifier other | BTSWXDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/111223 | |
| description abstract | Contains results of tunnel tests to determine effects of various combinations of split flaps, slats, and nose slats on the stability characteristics of a tapered 37.5 degree sweptback wing of aspect ratio 3 in straight and rolling flow. | |
| language | English | |
| title | NACA-RM-L8I03 | num |
| title | The effects of high-lift devices on the low-speed stability characteristics of a tapered 37.5 degree sweptback wing of aspect ratio 3 in straight and rolling flow | en |
| type | standard | |
| page | 30 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1948 | |
| contenttype | fulltext | |
| subject keywords | COMPLETE | |
| subject keywords | DAMPING | |
| subject keywords | DERIVATIVES | |
| subject keywords | DIRECTIONAL | |
| subject keywords | FLAPS | |
| subject keywords | LATERAL | |
| subject keywords | SLATS | |
| subject keywords | SLOTS | |
| subject keywords | STABILITY | |
| subject keywords | STATIC | |
| subject keywords | SWEEP | |
| subject keywords | WINGS |