درباره ما
NACA-TN-2445
Wind-tunnel tests at low speed of swept and yawed wings having various plan forms
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:58:12Z | |
| date available | 2017-09-04T15:58:12Z | |
| date copyright | 01/01/1951 | |
| date issued | 1951 | |
| identifier other | BFPTYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/61412 | |
| description abstract | Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptback, sweptforward, and yawed wings. The tests covered changes in aspect ratio, taper ratio, and tip shape. Some data were obtained with high-lift devices on sweptback wings and with ailerons on sweptforward wings. The data have been briefly analyzed and some comparisons have been made with the available theory. | |
| language | English | |
| title | NACA-TN-2445 | num |
| title | Wind-tunnel tests at low speed of swept and yawed wings having various plan forms | en |
| type | standard | |
| page | 83 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1951 | |
| contenttype | fulltext | |
| subject keywords | COMPLETE | |
| subject keywords | DESIGN | |
| subject keywords | DEVICES | |
| subject keywords | HIGH | |
| subject keywords | LIFT | |
| subject keywords | SWEEP | |
| subject keywords | VARIABLES | |
| subject keywords | WINGS |
