Application of the finite element method to study the dynamics of a helicopter
14th AIAA Aviation Technology, Integration, and Operations Conference
01.01.2014
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
APPLICATION OF THE FINITE ELEMENT METHOD TO STUDY THE DYNAMICS OF A HELICOPTER (AIAA 2014-3262)
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|Finite element analysis of helicopter structures
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|Improved Finite Element Modeling of Helicopter Airframe Connections
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|Development of an ACAP helicopter finite element impact model
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