Lateral stability analysis of frames for civilianaircraft structures
The fuselage of a civilian airplane is a quite complex structure build from slendermembers and panels. Slender members are essential to minimize the weight of theairplane. These slender structures are at risk of buckling due to high compressiveloads. The scope of this thesis is to evaluate the later...
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| Format: | Others |
| Language: | English |
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Linköpings universitet, Mekanik och hållfasthetslära
2017
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-147977 |