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Stresses around rectangular cut-outs in skin-stringer panels under axial loads - II /
Cut-outs in wings or fuselages produce stress concentrations that present a serious problem to the stress analyst. As a partial solution of the general problem, this paper presents formulas for calculating the stress distribution around rectangular cut-outs in axially loaded panels. The formulas are...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autores Corporativos: | , |
| Otros Autores: | , |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Langley Field, VA :
Langley Memorial Aeronautical Laboratory,
1943.
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| Colección: | NACA WR ;
L-368 |
| Temas: | |
| Acceso en línea: | Texto completo |