NACA-TN-4044
Ground effects on the longitudinal characteristics of two models with wings having low aspect ratio and pointed tips
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:11:41Z | |
| date available | 2017-09-04T18:11:41Z | |
| date copyright | 01/01/1957 | |
| date issued | 1957 | |
| identifier other | HAOUYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/194722 | |
| description abstract | Wind-tunnel tests were conducted to determine the ground effects on a tailless model with a wing of aspect ratio 2 and infinite taper, and on a tailed model with a triangular wing of aspect ratio 3, with flaps. Control-surface hinge moments were measured on the tailless model. The results are compared with the predictions of the theory of Tani, et al. | |
| language | English | |
| title | NACA-TN-4044 | num |
| title | Ground effects on the longitudinal characteristics of two models with wings having low aspect ratio and pointed tips | en |
| type | standard | |
| page | 49 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1957 | |
| contenttype | fulltext | |
| subject keywords | AIRPLANES | |
| subject keywords | COMBINATIONS | |
| subject keywords | COMPLETE | |
| subject keywords | CONTROL | |
| subject keywords | CONTROLS | |
| subject keywords | EDGE | |
| subject keywords | FLAP | |
| subject keywords | FLAPS | |
| subject keywords | FUSELAGE | |
| subject keywords | HINGE | |
| subject keywords | LONGITUDINAL | |
| subject keywords | MOMENTS | |
| subject keywords | STABILITY | |
| subject keywords | STATIC | |
| subject keywords | TAIL | |
| subject keywords | TRAILING | |
| subject keywords | TYPE | |
| subject keywords | WING | |
| subject keywords | WINGS |

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