Optimization of Helicopter Rotor Using Polynomial and Neural Network Metamodels
Author:
Affiliation:
1. Indian Institute of Science, Bangalore 560012, India
2. National Aerospace Laboratories, Bangalore 560012, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031156
Reference53 articles.
1. Renaissance of Aeroelasticity and Its Future
2. Helicopter Vibrations: A Technological Perspective
3. Application of Higher Harmonic Control to Rotors Operating at High Speed and Thrust
4. Wind Tunnel Results Showing Rotor Vibratory Loads Reduction Using Higher Harmonic Blade Pitch
5. Individual Blade Control Independent of a Swashplate
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