Deformation analysis of wing structures /
The elementary theories of bending and torsion often do not describe the stresses in aircraft shell structures with adequate accuracy; more refined stress theories have therefore have developed over a period of years. Theories of this nature are applied to the problem of calculating the deflections,...
Clasificación: | Libro Electrónico |
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Formato: | Documento de Gobierno Electrónico eBook |
Idioma: | Inglés |
Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947.
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Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1361. |
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Acceso en línea: | Texto completo |