首页 研究成果 发表论文 研究成果 发表论文 稀薄气体动力学理论与计算 1.Zhiqiang HE, Zhongzheng Jiang, Huangwei Zhang, Weifang Chen, Analytical method of nonlinear coupled constitutive relations for rarefied non-equilibrium flows. Chinese Journal of Aeronautics, 2020, 2020, 34(2): 136-153 2.He Z. Q., Fan G. C., Jiang Z. Z., Numerical application of the nonlinear coupled constitutive relations under three-dimensional hybrid unstructured finite-volume framework. International Journal of Modern Physics B, 2020: 2040071（2020.06） 3.Z. Yuan, Z. Jiang, W. Zhao, and W. Chen, Multiple temperature model of nonlinear coupled constitutive relations for hypersonic diatomic gas flows, AIP Advances 2020, 10: 055023（2020.05） 4.Z. Yuan, W. Zhao, Z. Jiang, W. Chen, and R. K. Agarwal, Modified Nonlinear Coupled Constitutive Relations Model for Hypersonic Nonequilibrium Flows, Journal of Thermophysics and Heat Transfer, 2020, 34(4): 848-859（2020.10） 5.Z. Yuan, Z. Jiang, W. Zhao, and W. Chen, Analysis of gas flow over a cylinder at all Knudsen numbers based on non-newtonian constitutive models, International Journal of Modern Physics B, 2020, 2040076（2020.6） 6.Jiang Z, Zhao W, Yuan Z, Chen W, et al. Computation of Hypersonic Flows over Flying Configurations Using a Nonlinear Constitutive Model. AIAA Journal, 2019: 57(12): 5252-5268（2019.12） 7.Jiang Z, Zhao W, Chen W, et al. An Undecomposed Hybrid Algorithm for Nonlinear Coupled Constitutive Relations of Rarefied Gas Dynamics. Communications in Computational Physics, 2019, 26: 880-912（2019.09） 8.Jiang Z, Zhao W, Chen W, et al. Computation of shock wave structure using a simpler set of generalized hydrodynamic equations based on nonlinear coupled constitutive relations. Shock Waves, 2019（2019.11） 9.江中正, 赵文文, 袁震宇, 陈伟芳. 基于非线性耦合本构关系的改进边界条件. 航空学报. 2018. 39 (10): 50-64 10.Zhongzheng Jiang, Weifang Chen, and Wenwen Zhao*. Numerical analysis of the micro-Couette flow using a non-Newton–Fourier model with enhanced wall boundary conditions, Microfuidics and Nanofuidics, 2018, 22(1): 1-20（2018.01） 11.赵文文，陈伟芳，邵纯等. 考虑多种物理效应的钝锥俯仰稳定性参数影响分析. 空气动力学学报. 2013(04): 442-448 12.赵文文, 姜婷婷, 陈伟芳. 尖锐前缘气动加热机理与激波脱体距离研究. 计算力学学报. 2013, 5: 733-737 13.赵文文，陈伟芳，邵纯等. 高超声速钝锥体俯仰阻尼导数影响因素分析. 国防科技大学学报. 2013(1): 43-47 14.Zhao W, and Chen W., Non-equilibrium Shock Structure Calculation with High-order Modified Navier-Stokes Equations, International Journal of Nonlinear Sciences and Numerical Simulation, 2013, 14(7-8): 493-500 15.Zhao W., Chen W., and Agarwal R., Formulation of a New Set of Simplified Conventional Burnett Equations for Computation of Rarefied Hypersonic Flows. Journal of Aerospace Science and Technology, 2014, 38: 64-75 16.Zhao W., Chen W., Liu H., Ramesh K., Computation of 1-D shock structure in a gas in rotational non-equilibrium using a new set of simplified Burnett equations, Vacuum, 2014, 109: 319-325 飞行器设计与优化 1.Xia C. and Chen W., Boundary-layer transition prediction using a simplified correlation-based model, Chinese Journal of Aeronautics, 2016, 29(1):66-75 2.Hua Yang, Lei Song, Weifang Chen. Research on parafoil stability using a rapid estimate model, Chinese Journal of Aeronautics, 2017, 30(5): 1670-1680 3.Chen-chao Xia, Ting-ting Jiang, and Wei-fang Chen, Particle Swarm Optimization of Aerodynamic Shapes with Nonuniform Shape Parameter-Based Radial Basis Function, Journal of Aerospace Engineering, 2017, 30(3): 04016089 4.夏陈超, 赵文文, 陈丽华, 陈伟芳. 高超声速压缩拐角湍流计算的收敛性分析. 航空动力学报, 2016, 21(2): 443-450 5.夏陈超, 陈伟芳, 郭中州等. 隐式紧耦合SST和TNT湍流模型的高速流动数值模拟. 航空动力学报, 2015, 30(4): 936-943 6.夏陈超, 姜婷婷, 郭中州, 陈伟芳. 压缩性修正对γ-Reθ转捩模型的影响研究. 空气动力学学报, 2015(5): 603-609 7.Chenchao Xia, Weifang Chen, Gradient-based Aerothermodynamic Optimization of a Hypersonic Wing Profile, Procedia Engineering, 2015, 126: 189-193（2015.05） 8.夏陈超, 邵纯, 姜婷婷等. 基于FFD方法的高超声速升力体气动优化. 固体火箭技术, 2015, 38(6): 751-756 流动稳定性、湍流与转捩 1.蔡林峰, 李昊歌, 陈伟芳. 无限展长后掠翼边界层定常横流不稳定转捩分析. 计算物理, 2019, 36(2): 175-181 2.蔡林峰,李昊歌,赵文文,陈伟芳. 简化三方程转捩模型在高超声速流动中的应用. 空气动力学学报, 2019, 37(6): 945-949, 982 3.蔡硕, 杨华, 陈伟芳. 展向上反角分布对飞翼布局横航向稳定性影响. 工业控制计算机, 2018, 31(5): 76-79 空气动力学实验与验证 1.Qiu Y L, Wu C J, Chen W F. Local heat transfer enhancement induced by a piezoelectric fan in a channel with axial flow. Journal of Zhejiang University-Science A: Applied Physics and Engineering, 2020, 21(12):1008-1022 2.Qiu Y L, Hu W J, Wu C J, et al. An experimental study of microchannel and micro-pin-fin based on-chip cooling systems with silicon-to-silicon direct bonding. Sensors, 2020, 20(19):5533 3.Qiu Y L, Hu W J, Wu C J, et al. Flow and heat transfer characteristics in a microchannel with a circular synthetic jet[J]. International Journal of Thermal Sciences, 2021, 164(3):106911 4.Qiu Y L, Wu C J. Numerical investigation of heat transfer enhancement in a slot channel induced by a piezoelectric fan. 2018 IEEE 13th Annual International Conference on Nano/Micro Engineered and Molecular Systems. Singapore, Singapore. IEEE, 2018 5.邱云龙, 胡文杰, 吴昌聚等. 嵌入式微通道液冷系统局部热点的传热特性与尺度效应研究. 浙大学报工学版 6.师昆仑, 邱云龙, 陈伟芳等. 传感器局部温度差异对压缩拐角热流测量的影响. 航空学报, 2021,42(3): 124055 非结构动网格与非定常流动 1.Guo Z Z, Dai G, Yang H, Chen W F. Unsteady flow simulation of a variable-sweep morphing aircraft coupled with flight control system. International Journal of Modern Physics B, 2020, 34(14-16): 2040073（2020.06） 2.郭中州, 何志强, 夏陈超, 陈伟芳. 高效计算网格壁面距离的KD树方法. 国防科大学报. 2017, 39 (4): 21-25 3.郭中州，何志强，赵文文，陈伟芳. 高效非结构网格变形与流场插值算法研究. 航空学报，2018, 39: 122411 4.郭中州，何志强，陈伟芳. 基于层次分析法和灰色关联分析法的非结构网格变形方法评价, 首届中国空气动力学大会. 2018.8.15-2018.8.19
