Variable Twist Blade with Piecewise Linear Twist Control for Rotor Power Reduction-Reference-Cited by-同舟云学术

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Variable Twist Blade with Piecewise Linear Twist Control for Rotor Power Reduction

Published:2019-01-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2019 Forum
language:
Short-container-title:

Author:

Zhang Xiaochi¹,Wan Zhiqiang¹,Yang Chao¹,Yan De¹

Affiliation:

1. Beihang University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1358

Reference17 articles.

1. Gessow, A. "Flight Investigation of Effects of Rotor-Blade Twist on Helicopter Performance," Technical Report NACA 1542, 1947.

2. Aeromechanics of a Slowed Rotor

3. Ramanujam, R., and Abhishek, A. "Performance Optimization of Variable-Speed and Variable-Geometry Rotor Concept." Journal of Aircraft ,2016: 1-14.

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