Helicopter Rotor-Blade Chord Extension Morphing Using a Centrifugally Actuated Von Mises Truss
Author:
Affiliation:
1. Mechanical Engineering Department, Swiss Federal Institute of Technology, Zurich 8092, Switzerland
2. Mechanical, Aerospace, and Nuclear Engineering Department, Rensselaer Polytechnic Institute, Troy, New York 12180
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032299
Reference6 articles.
1. Extendable Chord Rotors for Helicopter Envelope Expansion and Performance Improvement
2. Design of Extendable Chord Sections for Morphing Helicopter Rotor Blades
3. JohnsonT. “Bistable Devices for Morphing Rotor Blades,” Ph.D. Thesis, Pennsylvania State Univ., University Park, PA, 2010.
4. Über die Stabilitätsprobleme der Elastizitätstheorie
5. Energy Dissipation of a Bi-stable von-Mises Truss under Harmonic Excitation
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