Stress And Strength Analyses Of Ultra-Light Aircraft Fuselage
Ultra-light aircraft is a special kind of low-speed general aircraft. It is low weighted and small-sized however can depart and land without changing the structure of any parts. This thesis is the case study on the stress and strength analyses of an ultra-light aircraft fuselage about its performanc...
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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/54624/1/Stress%20And%20Strength%20Analyses%20Of%20Ultra-Light%20Aircraft%20Fuselage.pdf |