The purpose is to present a consistent finite-element formulation, developed to predict the free vibration characteristics of two different helicopters tailboom structures
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Updated
Feb 23, 2018 - TeX
The purpose is to present a consistent finite-element formulation, developed to predict the free vibration characteristics of two different helicopters tailboom structures
This is a report for homework during the course "Mechanical Design and Machine Elements" develop FEM analys
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