威尼斯娱人城官网

1979-1982, Ohio State UniversityUnited State, Doctor

2011- Current Chair Professor & Chief Scientist, School of Mechanical Engineering, SJTU
2002-2011 Principal Engineer-Aeromechanics, GE Aviation
2004-2010 Aeromechanics Consultant: Fan, LPC, HPC Design & Cert, GE Aviation
1999-2004 Fan, LPC, and HPC Aeromechanics Design Leader, GE Aviation
1994-2002 Senior Engineer, GE Aircraft Engine
1984-1994 Aeromechanics Engineer, GE Aircraft Engine
1982-1984 Principal Scientist, NASA Lewis Research Center, Cleveland, Ohio
1979-1982 Research Assistant, Dept. of Engineering Mechanics, Ohio State University

Turbofan Aeromechanics & Engine Dynamics
Certification for Airworthiness
Aviation Propulsion System Integration
Digitalization, Intelligent Design and Intelligent Life Management

I. Major Aeras
- HBP Fan Design & Certification
- Lighter Material HBP Fan Blade Design， Manufacture and Experimental Validation
- System Integration
II. University Collaboration
- Airworthy Infrastructure & Compliance Technology
III. Industry Collaboration
i) Genetic Engineering of Lighter Material HBP Fan
-From design, manufacture to Certification
ii) Engine and Aircraft Integration
-Installation & Inlet Compatibility
III. Cert Agency Collaboration
i) Reliability and Safety of Aviation Propulsion System
ii) Emerging Technology & Engine Safety
IV. Global Collaboration (Universities and Research Institutes)
-Unsteady Aerodynamics, Unsteady Aeroacoustics, and Unsteady Aeromechanics
V. R&D Projects in Progress:
i) From Genetic Engineering to System Integration
ii) Synthesis of Aviation Propulsion System – Compatibility & Operability
iii）PHM System & Intelligent Control & Fleet Management
iv）Implicit Science & Virtual Reality
v）Mutibody & Multimedia Engine Dynamics
Vi）Multi-Disciplinary Coupling Characteristics
(

Book
From Big Data to Intelligent Manufacture by Jay Lee, Nee Jun & AJ Wang
Shanghai Jiao Tong University Press 2016

As Advisor and Co-Author
1. Substructure-based distributed collaborative probabilistic analysis method for low-cycle fatigue damage assessment of turbine blade-disk. Aerospace Science and Technology, [1] Gao H. F, et al.
2. Substructure-based approach for probabilistic analysis of turbine blade low-cycle fatigue damage using moving least squares. IEEE Transactions on Reliability. Gao H. F, et al.
3. Reliability assessment framework on fatigue performance for turbo-fan blades under vibrational aerodynamic load. 29th European Safety and Reliability Conference, Gao H. F, et al.
4. Dynamic reliability assessment framework for turbine blades subject to low-cycle fatigue damage with variable-amplitude thermo-structural interaction. Engineering Failure Analysis. Gao H. F, et al.
5. An integrated reliability approach with improved importance sampling for LCF damage prediction of turbine disks with hyper-parameter. Gao H. F, et al.
6. A novel numerical approach on reliability assessment for turbine blades under the coupling LCF and HCF. Gao H. F, et al.
7. Numerical Investigation on Aeroelastic Behavior of Composite Material Plate Excited by Pulsed Air Jet[J]. Journal of Thermal Science, 2018(4):1-9. Xie H, et al.
8. Experimental Investigation on a Single NACA Airfoil’s Nonlinear Aeroelasticity in the Wind Tunnel under Aerodynamic Excitation[J]. Fluid dynamics, 2018-07, Xie H, et al.
9. Numerical Investigation of Inlet Distortion for Different Rear Mounted Engine Installations at Taking-Off Conditions[C]// ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. 2015:V001T01A009. Xie H, et al.
10. Numerical Investigation of Crosswind Effect on Different Rear Mounted Engine Installations[C]// ASME 2014 Gas Turbine India Conference. 2014:V001T01A006. Xie H, et al.
11. A NUMERICAL INVESTIGATION OF FAN BLADE/CASING RUB INDUCED VIBRATION AND ABRDABLE COATING REMOVAL, Proceedings of ASME Turbo Expo 2019: Xiao J., et al.
12. The analysis of composite blade/casing rub stability through delayed differential equations, Proceedings of ASME Turbo Expo 2019. Xiao J., et al.
13. Investigation of fan blades vibration due to blade/casing rubbing interactions using in-plane two-dimensional model. Proceedings of ASME Turbo Expo 2018: Xiao J., et al.
14. A general ply design for aero engine composite fan blade. Proceedings of ASME Turbo Expo 2017. Xiao J., et al.
15. Numerical Investigation on Wide-Chord Fan Blade Forced Response due to Vortex Ingestion. ASME. Turbo Expo 2018: Power for Land, Sea, and Air, Volume 7C: Structures and Dynamics ():V07CT36A016. doi:10.1115/GT2018-76352. Wang Z, et al.
16. 钛合金宽弦风扇叶片的振动特性. 航空动力学报，2018,33（11）：2593-3601. 王仲林，et al.
17. Inlet Compatibility and Fan Aeromechanics of HBP Turbofan Engine. ASME. Turbo Expo 2017: Power for Land, Sea, and Air, Volume 1: Aircraft Engine; Fans and Blowers; Marine; Honors and Awards ():V001T01A009. doi:10.1115/GT2017-63427. Wang Z, et al.
18. Stack Line Optimization Based on Vibration Characteristics of an Aero-engine Fan Blade. Journal of Aircraft. Wang Z, et al.
19. Investigation on the Dynamic Response of a Wide-Chord Fan Blade under Ground Vortex Ingestion. International Journal of Aeronautical and Space Sciences. Wang Z, et al.
20. Investigation on Vibration Characteristics of Titanium Wide-Chord Fan Blade under Three-Axial Excitation. Journal of Theoretical and Applied Mechanics. Wang Z, et al.
21. Dynamic thin-airfoil stall and leading-edge stall of oscillating wings at low Reynolds number 《Fluid dynamics》. Chengwei Fan, et al.
22. INVESTIGATION OF STALL FLUTTER OF FAN BLADES BY BLADE TIP-TIMING SYSTEM, , Proceedings of the 15th International Symposium on Unsteady Aerodynamics, Aeroacoustics & Aeroelasticity of Turbomachines ISUAAAT15 2018, University of Oxford, UK. Chengwei Fan, et al.
23. Analysis of blade tip timing data from fan blades with synchronous and non-synchronous vibration. 13th International Conference on Vibration Measurements by Laser and Noncontact Techniques AIVELA 2018, Ancona, Italy. Chengwei Fan, et al.
24. Nacelle, Air Intake Aerodynamic Design And Inlet Compatibility[C]// Asme Turbo Expo: Turbine Technical Conference & Exposition. 2015. Chen J, et al.
25. Numerical Investigation of Crosswind Effect on Different Rear Mounted Engine Installations[C]// Asme Gas Turbine India Conference. 2014. Chen J, et al.
26. 侧风条件下进气道流场及地面吸入涡特征研究，航空动力学报. 陈晶晶，等，
27. Detailed research on the characteristics of ground vortex under crosswind condition.(in process). Chen J, Wang A, et al.
28. Application of Proper Orthogonal Composition Method in Unsteady Flow Field Analysis of Axial Compressor.——Proceedings of ASME Turbo Expo 2019: Turbine Technical Conference and Exposition. Zhang Kai, et al.
29. Flow Field Analysis of Axial Compressor Rotor Near Stall Condition.
——Journal of Theoretical and Applied Mechanics. Zhang Kai, et al.

Lectures and Workshops Given:
Gas Turbine Fundamental
Genetic Engineering of HBP Turbofan
Lighter Material HBP Fan Blade Design Fundamental
Evolution of Aero Engine
Emerging Technologies and Challenges Ahead
From the Top: Introduction of System Engineering
Significance of Airworthy Certification
Implicit Science – Engine Dynamics，Operability and Compatibility
Inlet Compatibility of Installed Configuration at Complex Operating Environment
Multibody & Multimedia Engine Dynamics
Multi-Disciplinary Coupling Syndrome and Outlier
Applied Technologies of Aero Engine
I-4.0 and Big Data
Digitalization and AI
Virtual Inverse Engineering
The Advanced BTT System
Advanced Technologies for Life Management – PHM, CPS, and IMC
Probabilistic Design
Safety and Reliability of the Complex Aviation Propulsion System
Variation and Standardization – The six-sigma Process
Virtual Reality Technology of Aviation Propulsion System
Professionalism vs. Dataism

2001-2003 Adjunct Professor of Aerospace Engineering, University of Cincinnati
2012- Adjunct Professor of Aerospace Engineering, Zhongnan University