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Calculations of the effect of wing twist on the air forces acting on a monoplane wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1935 |
| Description | A method is presented for calculating the aerodynamic forces on a moncylane wing, taking into account the elastic twisting of the wing due to these forces. The lift distribution along the span is calculated by the formulas of Amstutz as a function of the geometrical characteristics of the wing and of the twist at stations 60 and 90 percent of the semispan. The twist for a given lift distribution is calculated by means of influence lines. As a numerical example, the forces on a Swiss military D.2V airplane are calculated. Comparisons with the strip method and with the ordinary stress-analysis method are also given. |
| File Size | 31756110 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930084824 |
| Archival Resource Key | ark:/13960/t6254t57v |
| Language | English |
| Publisher Date | 1935-01-01 |
| Access Restriction | Open |
| Subject Keyword | Formulas-lift Distribution-amstutz Wings-design & Theory Wings, Monoplane- Twisted Wings- Dewoitine 27 Lift Distribution, Wing Span-monoplanes Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
