王萌

Doctor of Engineering, Lecturer, Master's Supervisor. In 2020, he graduated from Harbin Engineering University with a doctor's degree in engineering. Since joining the workforce, I have been engaged in technical research and teaching related to marine gas turbine power plants for a long time. My main research areas include rapid simulation and prediction of aerodynamic performance of turbomachinery and testing methods, large-scale multiphase flow separation numerical simulation and testing technology, and ship power intake and exhaust guarantee. We have constructed a homogenization and high-precision prediction method for the intake flow field, breaking through the integrated design method for the intake and exhaust systems of highly compact and low detectable marine power plants. We have proposed a fast prediction method for large-scale spatiotemporal unsteady flow based on harmonic balance method, and achieved full three-dimensional rapid numerical simulation of major faults such as compressor surge.During my work, as the project leader, I undertook one National Natural Science Foundation Youth Fund project, one National Major Science and Technology Special Sub project, two horizontal scientific research projects, and one Central University Basic Research Fund. Led or participated in one of the National Natural Science Foundation's youth projects for multiple national research projects. Published over 20 papers in high-level journals both domestically and internationally, applied for 6 national invention patents, and published 1 academic monograph. Received one first prize for scientific and technological progress in Heilongjiang Province and one second prize for national defense scientific and technological progress.

2009/09-2012/06，Harbin Engineering University，        Marine Engineering，      Bachelor degree   
2013/09-2015/03，Harbin Engineering University，        Marine Engineering，      Master degree
2015/09-2020/06，Harbin Engineering University，        Marine Engineering，       Doctor Degree

2023.07-now Harbin Engineering University ,  Associate Professor
2020.07-2023.07 Harbin Engineering University, Lecture

Aerodynamic performance Prediction Method of Turbomachinary

《Mechanism and Characteristic of Laminar Separation Bubble in Turbomachinery with Adverse Pressure Gradient》

1. Wang Meng, Sun Haiou, Wang Zhongyi, Wang Yanhua, Magagnato Franco, Luan Yigang. Numerical investigation of the effects of system volume and average mass flow on the surge characteristics of an axial compressor[J]. Aerospace Science and Technology, 2020, 106. WOS:000579863200101
2. Liu Xiaogang, Qu Yonglei, Wang Yanhua, Wang Meng, Wang Zhongyi, Sun Haiou. Numerical analysis of two hollow drops simultaneously impacting a wet surface[J]. Physics of Fluids, 2021, 33(4). WOS:000639391700001
3. Haiou Sun, Meng Wang, Zhongyi Wang, Franco Magagnato. Numerical investigation of surge prediction in a transonic axial compressor with a hybrid BDF/Harmonic Balance Method[J]. Aerospace Science and Technology,2019,90, 401-409. 
4. Haiou Sun, Meng Wang, Zhongyi Wang, Jingyuan Ma. Numerical simulation of non-uniform roughness distribution on compressor performance[J]. Journal of Marine Science and Technology,2018,23(2), 389-397. 
5. Sun, Haiou, Meng Wang, Zhongyi Wang, Song Wang, and Magagnato Franco, Numerical simulation of the non-uniform flow in a full annulus multi-stage axial compressor with the harmonic balance method[J]. Advances in Mechanical Engineering, 2020, 12(3), 1-9. 
6. Zhongyi Wang,Jingyuan Ma,Song Wang,Meng Wang. Investigation on the effects of blade corrosion on compressor performance[J]. Journal of the Chinese Institute of Engineers,2016,39(7). 816-824. 
7. Franco Magagnato, Meng Wang, Zhongyi Wang, and Haiou Sun. Surge prediction of the NASA Stage 35 axial compressor by using a hybrid BDF/Harmonic balance method[C]. The 13th international symposium on experimental and computational aerothermodynamics of internal flows, Okinawa, Japan, 2017. 
8. Sun Haiou, Meng Wang, Zhongyi Wang, Song Wang, and Feng Qu. Numerical research on two-phase flow and erosion characteristic of axial compressor[C], The 13th international symposium on experimental and computational aerothermodynamics of internal flows, Okinawa, Japan, 2017.