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北京航空航天大学 [25]

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会议论文 [48]

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	Substructure-based flutter analysis for a wing-aileron system with freeplay 会议论文 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, 2018-01-08 作者: Xiangyu, W.; Zhigang, W.; Chao, Y.; Xufei, H. 收藏 \| 浏览/下载：7/0 \| 提交时间：2019/12/30 Aeroelasticity Ailerons Aviation Control nonlinearities Elastic waves Finite element method Flutter (aerodynamics) Frequency domain analysis Hopf bifurcation Nonlinear analysis Stiffness Structural analysis Structural dynamics Vibration analysis Aeroelastic system Bending stiffness Effective approaches Ground vibration tests Nonlinear aeroelasticity Nonlinear flutters Structural non-linearities Wing aileron system Time domain analysis
	Fast flutter uncertainty calculation based on arbitrary modal shapes and reduced - Order modeling 会议论文 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, 2018-01-08 作者: Guangjing, H.; Yuting, D.; Chao, Y.; Siyan, Z. 收藏 \| 浏览/下载：10/0 \| 提交时间：2019/12/30 Aeroelasticity Aviation Computational fluid dynamics Flutter (aerodynamics) Intelligent systems Modal analysis Monte Carlo methods Principal component analysis Structural analysis Structural dynamics Aerodynamic force coefficients Polynomial chaos expansion (PCE) Reduced order models Stiffness variations Structural parameter Structural variations Uncertainty calculations Uncertainty quantifications Uncertainty analysis
	A highly efficient aeroelastic analysis method based on external aerodynamic force and strip theory 会议论文 AIAA Aerospace Sciences Meeting, 2018, 2018-01-08 作者: Yan, Q.; Wan, Z. 收藏 \| 浏览/下载：14/0 \| 提交时间：2019/12/30 Aerodynamic loads Aerodynamics Aviation Computation theory Computational efficiency Efficiency A-plane Aerodynamic forces Aeroelastic analysis High-efficiency Strip theory Aeroelasticity
	Non-probabilistic stability reliability analysis of composite laminated panels in supersonic flow with uncertain-but-bounded parameters 会议论文 AIAA Non-Deterministic Approaches Conference, 2018, 2018-01-08 作者: Zheng, Y.; Qiu, Z. 收藏 \| 浏览/下载：24/0 \| 提交时间：2019/12/30 Aerodynamics Aeroelasticity Aviation Computation theory Eigenvalues and eigenfunctions Flutter (aerodynamics) Laminated composites Laminates Laminating Monte Carlo methods Numerical methods Reliability Stability Supersonic flow Uncertainty analysis Classical laminate theory Eigen-value Laminated panels Non-probabilistic reliability indices Statistical information Uncertain-but-bounded parameters Uncertainty Uncertainty propagation Reliability analysis
	Consideration of POD interpolation for aeroelastic design with large global structural variations use structural dynamic reanalysis 会议论文作者: Li, Dongfeng; Chen, Gang; Da Ronch, A.; Zhou, Qiang; Li, Yueming 收藏 \| 浏览/下载：15/0 \| 提交时间：2019/11/26 Aeroelastic response Approximate methods Flutter boundaries Proper orthogonal decompositions Reconstruction method Reduced order models Structural parameter Structural variations
	Control Mechanism of Aeroelastic System based on Piezoelectric Actuator 会议论文 PROCEEDINGS OF THE 2016 2ND INTERNATIONAL CONFERENCE ON ADVANCES IN ENERGY, ENVIRONMENT AND CHEMICAL ENGINEERING (AEECE 2016), 2016-01-01 作者: Sun, Jie; Li, Min 收藏 \| 浏览/下载：3/0 \| 提交时间：2019/12/30 aeroelasticity MFC negative velocity feedback additional aerodynamic force control mechanism
	Aerodynamic shape optimization and static aeroelastic analysis of a morphing trailing edge wing 会议论文 54th AIAA Aerospace Sciences Meeting 作者: Zhang, M.; Yang, C.; Wan, Z. 收藏 \| 浏览/下载：3/0 \| 提交时间：2019/12/30 Aerodynamics Aerospace engineering Airfoils Aviation Computational fluid dynamics Drag Fighter aircraft Interpolation Optimization Shape optimization Aero-dynamic performance Aerodynamic design optimization Aerodynamic shape optimization Aeroelastic constraints Genetic optimization algorithm Loosely coupled method Morphing trailing edges Parameterization method Aeroelasticity
	Control Mechanism of Aeroelastic System based on Piezoelectric Actuator 会议论文 2nd International Conference on Advances in Energy, Environment and Chemical Engineering (AEECE), SINGAPORE 作者: Sun, Jie; Li, Min 收藏 \| 浏览/下载：3/0 \| 提交时间：2019/12/30 aeroelasticity MFC negative velocity feedback additional aerodynamic force control mechanism
	A high-efficiency aeroelastic optimization method based on kriging model and genetic algorithm 会议论文 16th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015, Saint Petersburg, Russia, 2015-06-28 作者: Wang, Xiaozhe; Wan, Zhiqiang; Yang, Chao 收藏 \| 浏览/下载：3/0 \| 提交时间：2020/01/06
	The aeroelastic trim and static stability analysis of highly flexible aircraft 会议论文 16th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015, Saint Petersburg, Russia, 2015-06-28 作者: Rui, Hu; Changchuan, Xie; Yi, Liu 收藏 \| 浏览/下载：7/0 \| 提交时间：2020/01/06

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