Design Optimization of a Controllable Camber Rotor Airfoil
Author:
Affiliation:
1. Pennsylvania State University, University Park, Pennsylvania 16802
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.24476
Reference22 articles.
1. Rotors with Trailing Edge Flaps: Analysis and Comparison with Experimental Data
2. Hover Testing of Active Rotor Blade-Tips Using a Piezo-Induced Bending-Torsion Coupled Beam
3. Application of a New Compressible Time Domain Aerodynamic Model to Vibration Reduction in Helicopters Using an Actively Controlled Flap
4. Design Issues of a High-Stroke, On-Blade Piezostack Actuator for a Helicopter Rotor with Trailing-Edge Flaps
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