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Effect of hybrid composite materials on the dynamic characteristics of helicopter blades

โœ Scribed by E. G. Pak; V. N. Stekol'nikov; Yu. P. Ganyushkin; R. V. Ivannikova; V. N. Kestel'man

Publisher
Springer US
Year
1982
Tongue
English
Weight
436 KB
Volume
18
Category
Article
ISSN
1573-8922

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A ยฎnite element technique is used to investigate the free-vibration characteristics of rotating laminated composite blades. The structure is discretized using a multilayered degenerated-solid shell element. Because of the geometry and the loading, a geometrically non-linear analysis is required. The