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Composite helicopter blades contribute to a quieter cabin


Book ID
122831887
Publisher
Elsevier Science
Year
2013
Tongue
English
Weight
473 KB
Volume
57
Category
Article
ISSN
0034-3617

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A moderate deflection composite helicopt
โœ Peretz P. Friedmann; Bryan Glaz; Rafael Palacios ๐Ÿ“‚ Article ๐Ÿ“… 2009 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 379 KB

The compatibility between a composite beam cross-sectional analysis based on the variational asymptotic approach, and a helicopter rotor blade model which is part of a comprehensive rotorcraft analysis code is examined. It was found that the finite element cross-sectional analysis code VABS can be c