@inproceedings{dad4b1aa88684db893f7989a73a4884c,
title = "Fin-actuator system modeling and experimental validating for aeroelastic research",
abstract = "A fin-actuator system is designed for fundamental aeroelastic research mainly considering the effects of the actuator dynamics on the flutter characteristics of the fin. A plunge mode and a rotational mode are the critical modes naturally uncoupled. An actuator with a DC motor and a planetary gearhead is used to provide the elastic supports for the rotational mode. The main tasks of this paper are to model the actuator{\textquoteright}s dynamics and structural dynamics of the system and then complete the synthesized modeling. Continually, the models are validated by the dynamic stiffness testing of the actuator and the ground vibration testing of the structure. At last, an iterative v-g method in frequency domain is introduced to calculate the flutter boundary of the fin-actuator system.",
author = "Renjia Zhang and Zhigang Wu and Chao Yang",
note = "Publisher Copyright: {\textcopyright} 2015, American Institute of Aeronautics and Astronautics Inc. All rights Reserved.; 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015 ; Conference date: 05-01-2015 Through 09-01-2015",
year = "2015",
doi = "10.2514/6.2015-1861",
language = "英语",
series = "56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference",
}