Analysis of Rotorcraft Vibration Reduction Using a Center-of-Gravity Offset

Author:

YOSHIZAKI Yuji1,SUNADA Shigeru2

Affiliation:

1. Mitsubishi Heavy Industries, Ltd.

2. Department of Aerospace Engineering, Nagoya University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference25 articles.

1. 1) Bielawa, R. L.: Rotary Wing Structural Dynamics and Aeroelasticity, American Institute of Aeronautics and Astronautics, Inc., Renton, Virginia, 2006, pp. 239–274.

2. 2) Straub, F. and Charles, B.: Preliminary Assessment of Advanced Rotor/Control System Concepts (ARCS), Technical Report 90-D03, USA AVSCOM, 1990.

3. 3) Ormiston, R.: Aeroelastic Considerations for Rotorcraft Primary Control with On-Blade Elevons, American Helicopter Society 57th Annual Forum Proceedings, Washington, D.C., May 2001.

4. 4) Shen, J. and Chopra, I.: Actuation Requirements for a Swashplateless Helicopter Control System with Trailing-Edge Flaps, 43rd AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference and 10th AIAA/ASME/AHS Adaptive Structures Conference, AIAA-2002-1444, Denver, Colorado, April 22–25, 2002.

5. 5) Shen, J. and Chopra, I.: A Parametric Design Study for a Swashplateless Helicopter Rotor with Trailing-Edge Flaps, American Helicopter Society 58th Annual Forum, Montreal, Canada, June 11–13, 2002.

Cited by 2 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. The Effect of Rotorcraft CG Offset on Aerodynamic Stability Aiming to Obtain Vibration Reduction;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2023

2. Note on Auxiliary Substitution Measures of CG Offset Aiming for Rotorcraft Vibration Reduction;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2023

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