Optimal Design of the Active Twist for Helicopter Rotor Blades with C-Spar-Reference-Cited by-同舟云学术

Optimal Design of the Active Twist for Helicopter Rotor Blades with C-Spar

Published:2008-04-09 Issue:3-4 Volume:15 Page:325-334
ISSN:1537-6494
Container-title:Mechanics of Advanced Materials and Structures
language:en
Short-container-title:Mechanics of Advanced Materials and Structures

Author:

Barkanov E.,Gluhih S.,Kovalov A.

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science,General Mathematics,Civil and Structural Engineering

Link

http://www.tandfonline.com/doi/pdf/10.1080/15376490801907855

Reference15 articles.

1. Rodgers, J. P. and Hagood, N. W. “Design, manufacture and testing of an integral twist-actuated rotor blade,”. Proc. 8th Int. Adaptive Structures and Technology Conf.

2. Adaptive Blade Twist – calculations and experimental results

3. Riemenschneider, J., Keye, S., Wierach, des, P and Rochettes, H. M. Overview of the Common DLD/ONERA Project “Active Twist Blade” (ATB). Proc. 30th European Rotorcraft Forum. pp.22.1–22.9.

4. Analysis of an actively twisted rotor by multibody global modeling

5. On the modeling of integrally actuated helicopter blades

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