Higher-Harmonic Deployment of Trailing-Edge Flaps for Rotor-Performance Enhancement and Vibration Reduction
Author:
Affiliation:
1. Department of Aerospace Engineering, 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.C033335
Reference21 articles.
1. Helicopter rotor lift distributions for minimum-induced power loss
2. Optimum Two-Per-Revolution Inputs for Improved Rotor Performance
3. Assessment of Active Controls for Rotor Performance Enhancement
4. Investigation of Trailing-Edge Flap Gap Effects on Rotor Performance Using High-Fidelity Analysis
5. Computational Fluid Dynamics—Computational Structural Dynamics Analysis of Active Control of Helicopter Rotor for Performance Improvement
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2. Rotor Power Savings and Pitch-Link Load Reductions with Spanwise-Varying Active Camber Morphing;Journal of Aircraft;2024-05
3. Parameter Analysis of Active Flap Control for Rotor Aerodynamic Control and Design;International Journal of Aerospace Engineering;2023-06-29
4. An Experimental Study on Rotor Aerodynamic Noise Control Based on Active Flap Control;Aerospace;2023-01-27
5. Airfoil Dynamic Stall Model Suitable for Large Angle Deflection of a Trailing Edge Flap;Fluid Dynamics;2022-06
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