代表性论文专著
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.