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NACA-TM-654
Stresses Produced in Airplane Wings by Gusts
Year: 1932
Abstract: Accurate prediction of gust stress being out of the question because of the multiplicity of the free air movements, the exploration of gust stress is restricted to static method which must be based upon: 1) stress measurements in free flight; 2) check of design specifications of approved type airplanes. With these empirical data the stress must be compared which can be computed for a gust of known intensity and structure. This "maximum gust" then must be so defined as to cover the whole ambit of empiricism and thus serve as prediction for new airplane designs.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:11:24Z | |
| date available | 2017-09-04T17:11:24Z | |
| date copyright | 01/01/1932 | |
| date issued | 1932 | |
| identifier other | YSONEEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/134973 | |
| description abstract | Accurate prediction of gust stress being out of the question because of the multiplicity of the free air movements, the exploration of gust stress is restricted to static method which must be based upon: 1) stress measurements in free flight; 2) check of design specifications of approved type airplanes. With these empirical data the stress must be compared which can be computed for a gust of known intensity and structure. This "maximum gust" then must be so defined as to cover the whole ambit of empiricism and thus serve as prediction for new airplane designs. | |
| language | English | |
| title | NACA-TM-654 | num |
| title | Stresses Produced in Airplane Wings by Gusts | en |
| type | standard | |
| page | 56 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1932 | |
| contenttype | fulltext |