Load transfer in the stiffener-to-skin joints of a pressurized fuselage
Structural analyses are developed to determine the linear elastic and the geometrically nonlinear elastic response of an internally pressurized, orthogonally stiffened, composite material cylindrical shell. The configuration is a long circular cylindrical shell stiffened on the inside by a regular a...
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| Format: | Others |
| Language: | en |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/38131 http://scholar.lib.vt.edu/theses/available/etd-06062008-155607/ |