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	Multi-component Nonlinear Schrodinger Equations with Nonzero Boundary Conditions: Higher-Order Vector Peregrine Solitons and Asymptotic Estimates 期刊论文 OAI收割 JOURNAL OF NONLINEAR SCIENCE, 2021, 卷号: 31, 期号: 5, 页码: 52 作者: Zhang, Guoqiang; Ling, Liming; Yan, Zhenya \| 收藏 \| 浏览/下载：51/0 \| 提交时间：2021/10/26 Multi-component NLS equations Nonzero boundary conditions Lax pair Loop group method Darboux transform Higher-order vector Peregrine solitons Parity-time-reversal symmetry Governing polynomial Asymptotic estimates
	Viscous/inviscid interacting shear flow theory with inferences and their applications to CFD 会议论文 OAI收割 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014, National Harbor, MD, United states, January 13, 2014 - January 17, 2014 作者: Gao Z(高智); Shen YQ(申义庆); Zha GC 收藏 \| 浏览/下载：24/0 \| 提交时间：2017/05/27 Governing equations Interacting shear flow theory Orthogonal coordinates Parabolized navier-stokes (PNS) Shear turbulent flow Small-scale structures Viscous/inviscid interacting flow Wall-surface criteria
	A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文 OAI收割 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China Xi R.; Jia H. 收藏 \| 浏览/下载：67/0 \| 提交时间：2013/03/25 In this paper a strong coupled CFD-CSD method is developed to simulate the aeroelastic phenomena. The CFD solver is based on the finite-volume algorithm for the Navier-Stokes equations on unstructured grid. The CSD solver solves the aeroelastic governing equations in the modal space. Their coupling is realized by a dual-time method. The spring-based smoothing method is adopted to deform and regenerate the aerodynamic grid. Two test cases are selected to validate the authors' method for static and dynamic aeroelastity .The results of the simulation for the static aeroelastic problems of a missile wing show that the Lift Coefficient and Drag Coefficient are severally 7% and 5% lower than those don't consider the elasticity of the wing. The results for the flutter boundary prediction of the AGARD 445.6 wing have been proved much closer to the experiment than using the DLM. This method can describe the effects of fluid viscosity more exactly for highly nonlinear transonic flight conditions. The calculation has proved reliable in the subsonic regime but not accurate enough in the supersonic regime. 2011 IEEE.
	Correlation Analysis of Epoxy/Amine Resin Cure, Structure and Chemorheological Behavior in RTM Processes 期刊论文 OAI收割 polymer composites, 2011, 卷号: 32, 期号: 4, 页码: 648-656 Ding YY; Jia YX; Yang JY; He HD; Sun S; Shi TF 收藏 \| 浏览/下载：22/0 \| 提交时间：2012/06/11 TRANSFER MOLDING PROCESS WOVEN FIBER MATS NUMERICAL-SIMULATION GOVERNING EQUATIONS RACE-TRACKING COMPOSITES FLOWS VISCOSITY POLYMERS PREFORM
	Reactive Mold Filling in Resin Transfer Molding Processes with Edge Effects 期刊论文 OAI收割 journal of applied polymer science, 2009, 卷号: 113, 期号: 6, 页码: 3815-3822 Ding YY; Jia YX; Yang JY; Sun S; Shi TF; An LJ 收藏 \| 浏览/下载：23/0 \| 提交时间：2010/05/04 FINITE-ELEMENT-METHOD WOVEN FIBER MATS NUMERICAL-SIMULATION GOVERNING EQUATIONS CURING KINETICS RACE-TRACKING FLOWS COMPOSITES INJECTION VISCOSITY
	Enhancements of the simulation method on the edge effect in resin transfer molding processes 期刊论文 OAI收割 MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2008, 卷号: 478, 期号: 1-2, 页码: 384-389 作者: Yang, Junying; Jia, Yu Xi; Sun, Sheng; Ma, Dong Jun; Shi, Tong Fei \| 收藏 \| 浏览/下载：15/0 \| 提交时间：2019/04/09 Rtm Edge Effect Numerical Simulation Modified Governing Equations
	Vibration analysis of laminated shells using a refined shear deformation theory 期刊论文 OAI收割 Journal of Reinforced Plastics and Composites, 1998, 卷号: 17, 期号: 16, 页码: 1431-1449 作者: Ma BA; He JF 收藏 \| 浏览/下载：977/40 \| 提交时间：2009/08/03 Vibration Analysis Laminated Shells Shear Deformation Governing Equations Cylindrical Shells And Panels Circular Cylindrical-Shells Plates Thick Panels