Theoretical and empirical analyses of thick skinned swept wing panels
The validity of conventional skin and stringer type analyses is verified experimentally for a thick milled skin aircraft structure. The accuracy of solution is evaluated by comparing the strain energies in a mathematical model to that obtained experimentally from a wing panel of a high performance a...
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| Language: | en_US |
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Monterey, California. U.S. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/13261 |