A fully automated framework for helicopter rotor blades design and analysis including aerodynamics, structure, and manufacturing-Reference-Cited by-同舟云学术

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A fully automated framework for helicopter rotor blades design and analysis including aerodynamics, structure, and manufacturing

Published:2016-12 Issue:6 Volume:29 Page:1602-1617
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Vu Ngoc Anh,Lee Jae Woo,Le Tuan Phuong Nam,Nguyen Song Thanh Thao

Funder

National Foundation for Science and Technology Development

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference29 articles.

1. Numerical optimization of helicopter rotor aerodynamic performance in hover;Pape;Aerosp Sci Technol,2005

2. Morris AM, Allen CB. Development of generic CFD-based aerodynamic optimisation tools for helicopter rotor blades. Proceeding of 25th AIAA applied aerodynamics conference; 2007 June 25–28; Cavanaugh (MA). Reston: AIAA; 2007.

3. High-fidelity optimization framework for helicopter rotors;Imiela;Aerosp Sci Technol,2012

4. Integrated aerodynamic load/dynamic optimization of helicopter rotor blades;Chattopadhyay;J Aircr,1991

5. Multiobjective design optimization of helicopter rotor blades with multidisciplinary constraints;Chattopadhyay,1991

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