Aeroelastic Tailoring of Composite Couplings and Blade Geometry of a Helicopter Rotor Using Optimization Methods-Reference-Cited by-同舟云学术

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Aeroelastic Tailoring of Composite Couplings and Blade Geometry of a Helicopter Rotor Using Optimization Methods

Published:1997-07-01 Issue:3 Volume:42 Page:218-228
ISSN:2161-6027
Container-title:Journal of the American Helicopter Society
language:en
Short-container-title:j am helicopter soc

Author:

Ganguli Ranjan,Chopra Inderjit

Publisher

American Helicopter Society

Cited by 23 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Deep Neural Network Surrogates for Optimal Design of Helicopter Rotor;Transactions of the Indian National Academy of Engineering;2021-04-12

2. Aeromechanical Stability of a Bearingless Rotor Helicopter with Double-Swept Blades;Journal of Aircraft;2021-03

3. Design Methodology for Aeroelastic Tailoring of Additively Manufactured Lattice Structures Using Low-Order Methods;AIAA Journal;2019-11

4. Aeroelastic Tailoring using Additively Manufactured Lattice Structures;2018 Multidisciplinary Analysis and Optimization Conference;2018-06-24

5. Adaptive Composite Marine Propulsors and Turbines: Progress and Challenges;Applied Mechanics Reviews;2016-10-03

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