Stress And Aeroelastic Analyses Of Ultralight Aircraft Wing
This paper attempts to study a methodology stress analysis of an ultralight-aircraft’s wing structure imperiled to certain stress loads throughout the research. The analysis will cover static and flutter analysis of the wing’s structure. For static, it is more into lift distributions and the resulta...
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| Format: | Monograph |
| Language: | English |
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Universiti Sains Malaysia
2021
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| Online Access: | http://eprints.usm.my/54530/1/Stress%20And%20Aeroelastic%20Analyses%20Of%20Ultralight%20Aircraft%20Wing.pdf |