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NACA-TM-910
Measurements on a low-wing model in the rotating jet and comparison with flight measurements
Year: 1939
Abstract: The present report deals with six-component measurements in the small tunnel of the DVL on a model of the BFW-M 27b(sub 1), which were made to determine the effect of rolling and yawing on the air forces and moments. The wind was given a spiral motion by means of a rotating screen, the model being suspended in the conventional manner.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:11:26Z | |
| date available | 2017-09-04T18:11:26Z | |
| date copyright | 01/01/1939 | |
| date issued | 1939 | |
| identifier other | ADYIYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/194417 | |
| description abstract | The present report deals with six-component measurements in the small tunnel of the DVL on a model of the BFW-M 27b(sub 1), which were made to determine the effect of rolling and yawing on the air forces and moments. The wind was given a spiral motion by means of a rotating screen, the model being suspended in the conventional manner. | |
| language | English | |
| title | NACA-TM-910 | num |
| title | Measurements on a low-wing model in the rotating jet and comparison with flight measurements | en |
| type | standard | |
| page | 21 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1939 | |
| contenttype | fulltext |