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.
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,
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