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Classification of defects in honeycomb composite structure of helicopter rotor blades

✍ Scribed by M. Balaskó; E. Sváb; Gy. Molnár; I. Veres


Publisher
Elsevier Science
Year
2005
Tongue
English
Weight
594 KB
Volume
542
Category
Article
ISSN
0168-9002

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The aeroelastic phenomena of a composite rotor blade in hover is investigated using a finite element method. A large deflection type beam theory is used for the one-dimensional global deformation analysis of the hingeless, isolated rotor undergoing arbitrary large displacements and rotations, but sm