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Scientific Research
Bai Yuguang
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Associate Professor Supervisor of Doctorate Candidates Supervisor of Master's Candidates
Scientific Research
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Paper Publication...
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张胜, Bai Yuguang, Youwei Zhang, Zhao, Dan.Thermal-Aeroelastic Investigation of a Hypersonic Panel Vibration Based on a Developed MMC Method[J],AEROSPACE,2024,11(3)
王伟吉, Wei Qian, Bai Yuguang, Wang, Kunming.Numerical studies on the thermal-fluid-structure coupling analysis method of hypersonic flight vehicle[J],Thermal Science and Engineering Progress,2024,40
白瑜光, 张有为, 钱卫, 陈香言.高温作用下飞行器舱体的动力学特性分析[J],应用基础与工程科学学报,2017,25(6):1170-1182
Qian W., Bai Y., Wang D..Design, manufacture and frequency experiment of a novel flutter model for AGARD WING 445.6 with structure-similarity[A],2016
Bai Y., Qian W..Influence of the rhomboid zone on aeroelastic experiments of supersonic aircraft[A],2016
杨恺, 白瑜光, 朱强华, 高效伟.Numerical investigations of aero-heating for missile slots[J],Journal of Aerospace Engineering,2016,29(1):1-6
Patents
一种针对固定信息长度的LDPC编译码系统平台
一种用于超声速风洞全动舵面模型的多功能根肋
一种用于超声速风洞全动舵面模型的多功能根肋
一种高超声速颤振风洞试验模型的机身整流体结构
一种模拟全动舵面颤振模型弯扭支撑刚度的装置
Published Books
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Research Projects
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新兴领域发展与重点潜力研究, 其他, 2022/08/22-2022/12/09, 结题
大型柔性叶片的气弹稳定性机理及颤振预测与控制, 国家科技部, 2020/11/01, 在研
基于非介入策略的参数不确定车辆-结构耦合系统随机振动研究, 国家自然科学基金项目, 2017/08/17-2022/04/18, 结题
数值飞行器原型系统的综合验证及应用, 国家科技部, 2016/07/14, 在研
考虑几何非线性的大展弦比机翼气动弹性模型加工, 企事业单位委托科技项目, 2014/11/10, 结题
高可扩展全耦合空气动力学数值模拟软件, 国家“863”项目, 2015/07/10, 结题