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18:00 Poster session & drinks
Room 1.1
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18:00
Room 1.1
Poster session & drinks
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18:00
1 mins
Deep Reinforcement Learning for Aeroservoelastic Control of Unmanned Multi-Body Aircraft with Geometric Nonlinearities
Zhuolin Ying, Ying Bi, Zijian Zhu, Chen Zhu, Xiaoping Ma
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18:01
1 mins
Nonlinear Aeroelasticity Characteristics and Dynamics Response Analysis of Unmanned Multi-Body Aircraft
Zijian Zhu, Ying Bi, Chen Zhu, Zhuolin Ying, Jian Zhang
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18:02
1 mins
Fluid-structure interaction of supersonic membrane structures
Zexuan Yang, Faying Zhang, Chao Yang, Bing Feng NG, Zhigang Wu
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18:03
1 mins
Structural optimization of a high-aspect-ratio wing with post-flutter constraint
Zhiying Chen, Yang Meng, Zhiqiang Wan, Changchuan Xie, Chao Yang
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18:04
1 mins
A state-space rigid-elastic coupling aeroelastic model with geometrical accurate boundary condition
Nongyue Gao, Changchuan Xie, Chao An, Chao Yang
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18:05
1 mins
A CFD/CTD/CSD based aero-thermo-elastic framework for full-vehicle scale analysis
Liang Ma, Zhiqiang Wan, Xiaozhe Wang, Keyu Li, Chang Li, Longfei He
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18:06
1 mins
Aeroelastic optimization of commercial aircraft considering high-precision aerodynamic performance
Keyu Li, Chao Yang, Xiaozhe Wang, Zhiqiang Wan, Liang Ma, Chang Li
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18:07
1 mins
Testing and Analysis of a Simplified Nonlinear Horizontal Stabilator of an Aircraft
Nichoas Stathopoulos, Viresh Wickramasinghe, Devon Downes
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18:08
1 mins
Reduced order modeling analysis for flexible wing using a co-rotational beam element
Yali Shao, Changchuan Xie, Chao An, Duoyao Zhang, Yuhui Zhang
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18:09
1 mins
Research on nonlinear substructure method and aeroelastic analysis of large flexible aircraft
Rui Zhao, Chao An, Changchuan Xie
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18:10
1 mins
Hypersonic flutter analysis based on three-dimensional local piston theory
Gaozhan Wang, Changchuan Xie, Chenyu Liu, Chao An
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18:11
1 mins
Gust response analysis of supersonic aircraft based on three-dimensional piston theory
Chen Song, Changchuan Xie, Chenyu Liu, Yang Meng
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18:12
1 mins
Influence of nonlinear aerodynamic effects on high aspect ratio aircraft model
Álvaro Antonio García Quesada, Pedro José González Ramirez, Guilherme Chaves Barbosa, Gerrit Sybe Stavorinus, Flávio José Silvestre
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18:13
1 mins
Aeroelastic State space modeling for flight flutter test simulation using expanded mode shapes from Ground Vibration Test data
Hemalatha E, Gourav Kumar Dutta, Mohamed Nishad K, Pavan Kumar Dasari
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18:14
1 mins
Aerodynamic and aeroelastic analysis of propeller-wing system with a unified UVLM framework
Ruijie Niu, Changchuan Xie, Zhitao Zhang, Chao An
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18:15
1 mins
Measurement and Control System Design for Propeller-Wing System Experiments
Wei Wang, Zhitao Zhang, Changchuan Xie, Chao Yang, Kunhui Huang
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18:16
1 mins
On the preparation of a flexible real-time aircraft model for a flight simulator
Gefferson Silva, Bernd Boche, Hannes Wilke, Flavio Silvestre
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18:17
1 mins
Nonlinear aeroelastic response of strut-braced high aspect ratio wings
Fahed Mohd, Mohammadreza Amoozgar, Stewart McWilliams
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18:18
1 mins
Experimental And Numerical Activities For Aeroelastic Analysis Of An Aluminum Wing
Davide Mastrodicasa, Silvia Vettori, Massimiliano Chillemi, Alessandro Laurini, Aleli Sosa Chavez, Emilio Di Lorenzo, Karl Janssens
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18:19
1 mins
Mathematical method for prediction aeroelastic phenomena and multidisciplinary optimization lifting surfaces of flight vehicle at preliminary stage design
Oleh Havaza, Vitalii Sukhov, Ruslan Nikitin
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18:20
1 mins
Aeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack
Guo Li, Gongde Li, Yingyou Hou, Junlin Shen, Pu Xing, Chen Ji