Influence of Blade Geometric Parameters on Aeroelastic Response of a Helicopter Rotor System-Reference-Cited by-同舟云学术

Influence of Blade Geometric Parameters on Aeroelastic Response of a Helicopter Rotor System

Published:2013-07 Issue:3 Volume:26 Page:555-570
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Laxman Vaitla¹,Venkatesan C.²,Byun Yung Hwan³

Affiliation:

1. Assistant Professor, Dept. of Aerospace Engineering, Amrita University, Amrita Nagar, Coimbatore–641112 (TN), India; formerly, Postdoctoral Fellow, Dept. of Mechanical and Aerospace Engineering, Seoul National Univ., Gwanak-gu, Seoul 151-744, Korea (corresponding author).

2. Pandit Ramachandra Dwivedi Chair Professor, Dept. of Aerospace Engineering, Indian Institute of Technology (IIT), Kanpur–208 016 (UP), India.

3. Professor, Dept. of Aerospace Information Engineering, Konkuk Univ., 1 Hwayang-dong, Gwangjin-gu, Seoul 143-701, Korea.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000168

Reference28 articles.

1. Bhagwat M. J. and Ormiston R. A. (2007). “Application of CFD/CSD coupling for analysis of rotorcraft airloads and blade loads in maneuvering light.” Proc. 63rd Annual Forum of the American Helicopter Society American Helicopter Society Alexandria VA.

2. Bir G. and Chopra I. (1993). “Aeromechanical stability of rotorcraft with advanced geometry blades.” Proc. 34th AIAA Structures Structural Dynamics and Materials Conf. American Institute of Aeronautics and Astronautics Reston VA.

3. Bousman W. G. (1999). “Putting the aero back into aeroelasticity.” Proc. 22nd Annual Workshop on Aeroelasticity of Rotorcraft Systems University Park PA.

4. Review of Rotor Loads Prediction with the Emergence of Rotorcraft CFD

5. Rotary-Wing Aeroelasticity: Current Status and Future Trends

Cited by 3 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. Dynamic analysis of a helicopter blade subjected to the aerodynamic loads based on Euler-Bernoulli beam theory;Australian Journal of Mechanical Engineering;2021-04-26

2. Parametric Analysis of a Large-Scale Cycloidal Rotor in Hovering Conditions;Journal of Aerospace Engineering;2017-01

3. Effects of blade configuration parameters on helicopter rotor structural dynamics and whirl tower loads;The Aeronautical Journal;2016-02