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Numerical simulation and transonic wind-tunnel test for elastic thin-shell structure considering fluid–structure interaction
作者姓名:Yan Yunju  Xi Zhuyou  Zhang Shanzhi
作者单位:School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University;College of Science, Liaoning University of Technology
基金项目:This study was supported by the National Natural Science Foundation of China,Specialized ,Research Fund (priority development area) for the Doctoral Program of Higher Education of China
摘    要:Aerodynamic force can lead to the strong structural vibration of flying aircraft at a high speed. This harmful vibration can bring damage or failure to the electronic equipment fixed in aircraft. It is necessary to predict the structural dynamic response in the design course. This paper presents a new numerical algorithm and scheme to solve the structural dynamics responses when considering fluid–structure interaction(FSI). Numerical simulation for a free-flying structural model in transonic speed is completed. Results show that the small elastic deformation of the structure can greatly affect the FSI. The FSI vibration tests are carried out in a transonic speed windtunnel for checking numerical theory and algorithms, and the wind-tunnel test results well accord with that of the numerical simulation. This indicates that the presented numerical method can be applied to predicting the structural dynamics responses when containing the FSI.

关 键 词:Aerodynamic  forces  Fluid–structure  interaction  Numerical  analysis  Thin  shells  Wind-tunnel  tests

Numerical simulation and transonic wind-tunnel test for elastic thin-shell structure considering fluid-structure interaction
Yan Yunju,Xi Zhuyou,Zhang Shanzhi.Numerical simulation and transonic wind-tunnel test for elastic thin-shell structure considering fluid-structure interaction[J].Chinese Journal of Aeronautics,2015,28(1):141-151.
Authors:Yan Yunju  Xi Zhuyou  Zhang Shanzhi
Institution:a School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi''an 710129, China;
b College of Science, Liaoning University of Technology, Jinzhou 121001, China
Abstract: Simulation-based training is a promising way to train a carrier flight deck crew because of the complex and dangerous working environment. Quantitative evaluation of simulation-based training quality is vital to make simulation-based training practical for aircraft carrier marshalling. This paper develops a personal computer-based aircraft carrier marshalling simulation system and a cave automatic virtual environment (CAVE)-based immersive environment. In order to compare the training effectiveness of simulation-based training and paper-based training, a learning cubic model is proposed and a contrast experiment is carried out as well. The experimental data is analyzed based on a simplified Kirkpatrick''s model. The results show that simulation-based training is better than paper-based training by 26.80% after three rounds of testing, which prove the effectiveness of simulation-based aircraft carrier marshalling training.
Keywords:Aerodynamic forces  Fluid-structure interaction  Numerical analysis  Thin shells  Wind-tunnel tests
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