陈树生


的个人主页 http://teacher.nwpu.edu.cn/911C0DC448D04697E053640A280A3E00

基本信息 The basic information

陈树生

航空学院

博士研究生毕业

工学博士

副教授

航空宇航科学-飞行器设计,力学-空气动力学,力学-流体力学

sshengchen@nwpu.edu.cn

工作经历 Work Experience

2019.08 - 至今, 西北工业大学航空学院, 副教授

2020.09 - 至今, 航空工业一飞院和西北工业大学, 博士后

教育经历 Education Experience

2014.09 - 2019.06,北京航空航天大学,博士

2010.09 - 2014.07,北京航空航天大学,学士


教育教学 Education And Teaching

(1) 本科生课程:《飞行动力学》和《蓝天翱翔-展翅高飞》;研究生课程:《高等飞行动力学》

(2) 指导大学生创新创业训练项目、顶峰计划、“飞鲨杯”中国研究生未来飞行器创新大赛

(3) 指导本科毕业设计论文6人,1人次“优秀本科毕业设计论文”和1人次“优秀毕业生”

(4) 指导研究生7人

招生信息 Admission Information

课题组长期招收从事计算流体力学、飞行动力学、气动设计、高超声速空气动力学、新概念飞行器设计研究工作的研究生,欢迎感兴趣的同学联系报考!


科学研究 Scientific Research

主要从事的研究方向:

1. 计算流体力学及气动设计

2. 超声速/高超声速空气动力学

3. 新概念飞行器设计及飞行动力学


主持科研项目:

XXX飞行器布局研究,装备预先研究领域基金项目。

XXX先进布局研究,装发技术项目。

XXX飞行器设计,军委科技委项目。

结合机器学习的XXX气动热计算方法研究,航天科学技术基金项目。

高超声速一体化飞行器XXX流动预测技术研究,陕西省自然科学基础研究计划(青年项目)。

超声速客机声爆XXX关键技术研究,军事科学院空气动力试验基地。

XXX垂直起降气动设计及总体优化,航空工业618所。

高超声速飞行器XXX控制机理研究,北京临近空间飞行器系统工程研究所

倾转旋翼飞行器XXX数值模拟研究,中央高校基本科研业务费。



学术成果 Academic Achievements

顾奕然,黄江涛,陈树生*,刘德园,高正红,基于逆向增广Burgers方程的声爆反演技术研究,航空学报, 43 (2022) 626258. 

舒博文,杜一鸣,高正红,夏露,陈树生*典型航空分离流动的雷诺应力模型数值模拟,航空学报, 43 (2022) 126385. 

S.-S. Chen, F.-J. Cai, X.-H. Xiang, Z.-H Gao, C. Yan, A low-diffusion robust flux splitting scheme towards wide-ranging Mach number flows, Chinese Journal of Aeronautics, 34 (2021) 628-641.(SCI)

C. Pang, Z.-H. Gao, H. Yang, S.-S. Chen*, An efficient grid assembling method in unsteady dynamic motion simulation using overset grid, Aerospace Science and Technology, 110 (2021) 106450. (SCI)

S.-S. Chen, Z. Li, W. Yuan, H.-F. Yu, C. Yan, Investigations on high-fidelity low-dissipation scheme for unsteady turbulent separated flows, Aerospace Science and Technology, 115 (2021) 106785. (SCI)

S.-S. Chen, B.-X. Lin, Y.-S. Li, C. Yan, HLLC+: LOW-MACH SHOCK-STABLE HLLC-TYPE RIEMANN SOLVER FOR ALL-SPEED FLOWS, SIAM Journal on Scientific Computing, 42 (2020) B921-B950. (SCI)

S.-S. Chen, F.-J. Cai, H.-C. Xue, N. Wang, C. Yan, An improved AUSM-family scheme with robustness and accuracy for all Mach number flows, Applied Mathematical Modelling, 77 (2020) 1065-1081. (SCI)

S.-S. Chen, C. Yan, B.-X. Lin, L.-Y. Liu, J. Yu, Affordable shock-stable item for Godunov-type schemes against carbuncle phenomenon, Journal of Computational Physics, 373 (2018) 662-672. (SCI)

S.-S. Chen, C. Yan, K. Zhong, H.-C. Xue, E.-L. Li, A novel flux splitting scheme with robustness and low dissipation for hypersonic heating prediction, International Journal of Heat and Mass Transfer, 127 (2018) 126-137. (SCI)

S.-S. Chen, C. Yan, B.-X. Lin, Y.-S. Li, A new robust carbuncle-free Roe scheme for strong shock, Journal of Scientific Computing, 77 (2018) 1250-1277. (SCI)

S.-S. Chen, C. Yan, X.-H. Xiang, Effective low-Mach number improvement for upwind schemes, Computers and Mathematics with Applications, 75 (2018) 3737-3755. (SCI)

S.-S. Chen, C. Yan, S. Lou, B.-X. Lin, An improved entropy-consistent Euler flux in low Mach number, Journal of Computational Science, 27 (2018) 271-283. (SCI)

S.-S. Chen, H. Yang, F.-J. Cai, Z.-H. Gao, Multi-dimensional dissipation strategy within advection upstream splitting methods in hypersonic flows, 2020 The 11th Asia Conference on Mechanical and Aerospace Engineering, 2020. (EI)

Shusheng Chen, Chao Yan, Boxi Lin, Erlong Li, An improved low-dissipation AUSMPW+ scheme for low Mach number, The 8th International Conference on Mechanical and Aerospace Engineering, (2017) 522-526. (EI)

S.-S. Chen, H. Yang, Z. Li, Z.-H. Gao, Pressure diffusion item to improve shock robustness for low-diffusion upwind schemes, 2021 12th International Conference on Mechanical and Aerospace Engineering, 2021. (EI)

陈树生, 刘丽媛, 阎超, 林博希, CFD软件自动化验证确认云平台设计与实现, 航空学报, 38 (2017) 120209. (EI)

J.-P. Li, S.-S. Chen, F.-J. Cai,  S. Wang, C. Yan, Bayesian uncertainty analysis of SA turbulence model for supersonic jet interaction simulations, Chinese Journal of Aeronautics, 2021. (SCI)

J.-P. Li, F.-Z. Zeng, S.-S. Chen, K.-L. Zhang, C. Yan, Bayesian model evaluation of three k–ω turbulence models for hypersonic shock wave–boundary layer interaction flows, Acta Astronautica, 189 (2021) 143-157. (SCI)

S. Lou, S.-S. Chen, B.-X. Lin, J. Yu, C. Yan, Effective high-order energy stable flux reconstruction methods for first-order hyperbolic linear and nonlinear systems, Journal of Computational Physics, 414 (2020), 109475. (SCI)

K. Zhong, C. Yan, S.-S. Chen, T.-X. Zhang, S. Lou, Aerodisk effects on drag reduction for hypersonic blunt body with an ellipsoid nose, Aerospace Science and Technology, 86 (2019) 599-612. (SCI)

K. Zhong, C. Yan, S.-S. Chen, X.-Y. Wang, S.-J. Jun, Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules, Acta Astronautica, 157 (2019) 189-198. (SCI)

Boxi Lin, Chao Yan, Shusheng Chen, Density enhancement mechanism of upwind schemes for low Mach number flows, Acta Mechanica Sinica, 34 (2018) 431-445. (SCI)

Boxi Lin, Chao Yan, Shusheng Chen, A study on the behavior of high-order Flux Reconstruction method with different low-dissipation numerical fluxes for Large Eddy Simulation, International Journal of Computational Fluid Dynamics, 31 (2017) 339-361. (SCI)

Boxi Lin, Chao Yan, Shusheng Chen, Study of A High-Order Flux Reconstruction Formula with Different Low-Dissipation Euler Fluxes at Low Mach Flow, The 8th International Conference on Mechanical and Aerospace Engineering, (2017) 472-477. (EI)

余华峰, 刘宏康, 陈树生, 阎超, X-51A飞行器非定常湍流精细模拟, 北京航空航天大学学报, 45 (2019) 624-632. (EI)

Yongkang Zheng, Yue Zhou, Shusheng Chen, Chao Yan, Application of a New Shock-Stable Scheme for Supersonic Combustion Flows, The 10th International Conference on Mechanical and Aerospace Engineering, (2019) 428-433. (EI)

Lin Bo-xi, Zhang Liang, Chen Shu-sheng, Li Bing, Jiang Zhen-hua, An Efficient Implicit High-order Flux Reconstruction Method by Automatic Differentiation using Operator Overloading for Flow Simulation on Unstructured Hexahedral Grids, The 10th International Conference on Mechanical and Aerospace Engineering, (2019) 164-170. (EI)

J. Yu, C. Yan, Z. Jiang, W. Yuan, S.-S. Chen, Adaptive non-intrusive reduced order modeling for compressible flows, Journal of Computational Physics, 397 (2019) 108855. (SCI)

Z.-J. Liu, Y.-T. Zhao, S.-S. Chen, C. Yan, F.-J. Cai, Predicting distributed roughness induced transition with a four-equation laminar kinetic energy transition model, Aerospace Science and Technology, 99 (2020) 105736. (SCI)

森林,高正红,朱新奇,庞超,杜一鸣,陈树生.非稳定动态过程非定常气动力建模航空学报, 2020, 41(8): 123675. (EI)

向星皓,张毅锋,陈坚强,袁先旭,陈树生. 横流转捩模型参数不确定度量化分析与应用研究宇航学报,2020, 41(9): 1141-1150. (EI)

J.-P. Li, S.-S. ChenF.-J. Cai,  C. Yan, Numerical investigation of vented plume into a supersonic flow in the early stage of rocket hot separation, Aerospace Science and Technology, 107 (2020) 106249. (SCI)

C. Pang, H. Yang, Z.-H. Gao, S.-S. ChenEnhanced adaptive mesh refinement method using advanced vortex identification sensors in wake flow, Aerospace Science and Technology, 115 (2021) 106796. (SCI)


社会兼职 Social Appointments

中国力学学会会员、中国航空学会会员

受邀担任JCP、AIAA J、AST、CAMWA、POF等多个期刊审稿人和多个国际、国内学术会议的分会主席或技术委员会成员