毛歅博
助理教授
同济大学航空航天与力学学院
电子邮箱:22206@tongji.edu.cn
2008.9-2012.6,南京航空航天大学,飞行器动力工程, 学士/ B.Sc.
2012.8-2013.12,Syracuse University,机械与航空工程,硕士/ M.Sc.
2014.5-2018.5,Syracuse University, 机械与航空工程,博士/Ph.D.
2017.6-2018.6,SoftInWay Inc,Software Application,Application Engineer
2019.4-2022.1,清华大学,能源与动力工程系,博士后
2022.9至今,同济大学,航空航天与力学学院,助理教授
1.流体力学与气动热力学
2.航空推进
3.叶轮机械
CFD分析软件应用
1.Mao Y, Dang T Q, A Three-Dimensional Body-Force Model for Nacelle-Fan Systems Under Inlet Distortions [J]. Aerospace Science and Technology (Q1), 2020, Vol. 106, 106085. https://doi.org/10.1016/j.ast.2020.106085
2.Mao Y, Su X, Yuan X, An Off-Design Flow Angle Model Based on Average-Flow Theory and Wake Analysis [J]. Journal of Thermal Science (Q2), 2023, https://doi.org/10.1007/s11630-023-1774-2.
3.Chen Z, Mao Y, Hu K, Su X, Yuan X, Theoretical Model for Two-Dimensional Film Cooling Effectiveness Distribution Prediction [J], Physics of Fluids, 2021, Vol. 34, Issue 2, pp. 025122.
4.Chen Z, Mao Y, Hu K, Su X, Yuan X, 2-D Prediction Method for Multi-Row Film Cooling Effectiveness [J]. Applied Thermal Engineering, 2021, Vol. 199, pp. 117607
1.Mao Y, Dang T Q, Simple Approach for Modeling Fan Systems with a Computational-Fluid-Dynamics-Based Body-Force Model [J]. Journal of Propulsion and Power (Q2), 2020, Vol. 36, Issue 5, pp. 642-654. https://doi.org/10.2514/1.B37742
2.Mao Y, Dang T Q, A Three-Dimensional Body-Force Model for Nacelle-Fan Systems Under Inlet Distortions [J]. Aerospace Science and Technology (Q1), 2020, Vol. 106, 106085. https://doi.org/10.1016/j.ast.2020.106085
3.Mao Y, Chen Z, Li H, Su X, Yuan X, On the Relation between Blade Loading and In-Passage Flow Field [J], Aerospace (Q2), 2021, Volume 8, Issue 11, pp. 324. https://doi.org/10.3390/aerospace8110324
4.Mao Y, Su X, Yuan X, A Novel Model for CFD-Based Throughflow Analysis of Film-Cooled Turbine Blade [J]. Journal of Thermal Science (Q2), 2022. https://doi.org/10.1007/s11630-022-1579-8
5.Mao Y, Su X, Yuan X, An Off-Design Flow Angle Model Based on Average-Flow Theory and Wake Analysis [J]. Journal of Thermal Science (Q2), 2023, https://doi.org/10.1007/s11630-023-1774-2.
6.Chen Z, Mao Y, Hu K, Su X, Yuan X, Theoretical Model for Two-Dimensional Film Cooling Effectiveness Distribution Prediction [J], Physics of Fluids, 2021, Vol. 34, Issue 2, pp. 025122.
7.Chen Z, Mao Y, Hu K, Su X, Yuan X, 2-D Prediction Method for Multi-Row Film Cooling Effectiveness [J]. Applied Thermal Engineering, 2021, Vol. 199, pp. 117607
8.Zhang Z, Mao Y, Su X, Yuan X, Adjoint-Based Boundary Condition Sensitivity Analysis [J]. AIAA Journal, 2022, Article in Advance.
9.Chen Z, Hu K, Mao Y, Su X, Yuan X, Interaction Mechanism and Loss Analysis of Mixing between Film Cooling Jet and Passage Vortex [J]. Entropy, Vol. 24, Issue 1, pp. 16.
10.Chen Z, Hu K, Mao Y, Su X, Yuan X, Simple Integral Model for Trajectories of Jet Deflection in Crossflow [J]. Physics of Fluids, 2021, Vol. 33, Issue 11, pp. 111703.
1.2023/11-2024/09(横向)透平叶片长周期衰退特性仿真验证
2.2023/02-2023/12(横向)航空发动机稳定性仿真建模与程序优化
3.2023/07-2023/12(横向)汽轮机模型测试