Calculation of lateral forces acting onto aircraft fuselage /
The design of an aircraft involves various stages that at all these stages, adequate structural sterngth and stiffness analysis is required of the main components. this will enable the aircraft to perform its intended role at expected level. The aim of this project is to analyse the loading action o...
Main Author: | 395152 Yeow, Yiew Loy |
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Published: |
Sekudai : UTM,
1993
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