Experimental study of structural damping of composite helicopter blades with different cores-Reference-Cited by-同舟云学术

Experimental study of structural damping of composite helicopter blades with different cores

Published:2010-02 Issue:1 Volume:39 Page:1-5
ISSN:1465-8011
Container-title:Plastics, Rubber and Composites
language:en
Short-container-title:Plastics, Rubber and Composites

Author:

Rasuo B.

Publisher

Informa UK Limited

Subject

Materials Chemistry,Polymers and Plastics,General Chemical Engineering,Ceramics and Composites

Link

http://www.tandfonline.com/doi/pdf/10.1179/174328910X12608851832092

Reference8 articles.

1. A. A. Baker, S. Dutton and D. Kelly (eds.): ‘Composite materials for aircraft structures’, 2nd edn; 2004, New York, AIAA.

2. High Damping Composite Materials: Effect of Structural Hierarchy

3. B. Rasuo: ‘Design, fabrication and testing of the helicopter tail rotor blade from composite laminated materials’, Proc. 13th Int. Conf. on ‘Composite materials’, Beijing, China, June 2001, International Committee on Composite Materials, Paper ID 1207.

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