Design of Flexible Propellers with Optimized Load-Distribution Characteristics-Reference-Cited by-同舟云学术

Design of Flexible Propellers with Optimized Load-Distribution Characteristics

Published:2014-01 Issue:1 Volume:51 Page:117-128
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Sodja Jurij¹,Drazumeric Radovan¹,Kosel Tadej¹,Marzocca Pier²

Affiliation:

1. Laboratory for Aeronautics, University of Ljubljana, Ljubljana 1000, Slovenia

2. Mechanical and Aeronautical Engineering Department, Clarkson University, Potsdam, New York 13699

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032131

Reference15 articles.

1. RosenA.FriedmannP. P. “Nonlinear Equations of Equilibrium for Elastic Helicopter or Wind Turbine Blades Undergoing Moderate Deformation,” NASA CR-159478, 1978.

2. HodgesD. H.DowellE. H. “Nonlinear Equations of Motion for the Elastic Bending and Torsion of Twisted Nonuniform Twisted Blades,” NASA TN-D-7818, 1974.

3. Influence of wind turbine flexibility on loads and power production

4. Aeroelastically adaptive propeller using blades’ root flexibility

5. Passively Varying Pitch Propeller for Small UAS

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