shi yong qiang


http://teacher.nwpu.edu.cn/en/shiyongqiang

The basic information

shi yong qiang

School of Power and Energy

Postgraduate

Doctor

Associate Professor

yqshi@nwpu.edu.cn

Education Experience

2005.09 – 2011.09  School of Power and EnergyNorthwestern Polytechnical University

Ph.D in Propulsion Theory and Engineering of Aeronautics and Astronautics

2003.09 – 2006.04  School of Power and EnergyNorthwestern Polytechnical University

M.A. in Propulsion Theory and Engineering of Aeronautics and Astronautics

1999.09 – 2003.07   School of Power and EnergyNorthwestern Polytechnical University

B.A. in Aircraft Power Engineering.

Work Experience

2014.05 – Present    Associate Profressor in School of Power and Energy, Northwestern Polytechnical University, Xi’an

Research areas:    Numerical & experimental Study on Flutter in Turbomachinery; Research and Development of Calculation Code for Unsteady flow in Multi-Stage Turbomachines; Fluid-Structure Coupling Method; Development and Application of Optimation Method in Aero-engine Design; Air Inlet and Exhaust System Design and Analysis; Aero-engine Stealth Design

2008.05 – 2014.04    Lecturer in School of Power and Energy, Northwestern Polytechnical University, Xi’an

Research areas:    Numerical & experimental Study on Flutter in Turbomachinery; Research and Development of Calculation Code for Unsteady flow in Multi-Stage Turbomachines; Fluid-Structure Coupling Method; Numerical Analysis of Flutter for Wide-chord Hollow Fan Blade; Development and Application of Optimation Method in Aero-engine Design

2006.05 – 2008.04    Assisant in School of Power and Energy, Northwestern Polytechnical University, Xi’an

Research areas:   Numerical Study on Unsteady flow in Cascade; Investigation of the Flutter Prediction Technology for Turbomachinery; Numerical Solution on Flow Field in high bypass ratio separate-flow  Exhaust Nozzle.

Scientific Research

Research Project


2014 – 2016:    Analysis of aeroelastic problems in Multistage turbomachines by harmonic balance methocd

Supported by National Science Foundation of China (No. 11302179), Grant holder

2013 – 2014:     Aeroelastic analysis of wide-chord hollow fan blade

Support by the Ph.D. Programs Foundation of Ministry of Education of China (No.20126102120042), Grant holder

2013 – 2014:     Investigation on a fast analysis method for nonlinear unsteady flows in turbomachinery

Support by Natural Science Basic Research Plan in Shaanxi Province of China(No.2013JQ1009), Grant holder

2012 – 2013:     Investigation on nonlinear analysis method for unsteady flow in turbomachinery

Supported by NPU Foundation for Fundamental Research (No.JC201245), Grant holder

 

PUBLICATIONS


[1]     Shi Yongqiang, Yang Qingzhen, Huang Xiuquan and Guo Xiao. A numerical approach for fast simulation of unsteady flow around oscillating cascades. ACTA AERODYNAMICA SINICA. Vol. 32(4): 481-487, 2014. (In Chinese)

[2]     Shi Yongqiang, Wang Yang and Yang Qingzhen. Design Optimization of Blade's Stacking Line Based on Fluid-Structure Coupling Technique. Applied Mechanics and Materials Vol. 459 (2014) pp 499-504.(EI:20134717004989) (In English)

[3]     Shi Yongqiang, Yang Qingzhen and Huang Xiuquan. Numerical Analysis of Three-Dimensional Unsteady Flows Around Oscillating Cascades Using Harmonic Balance Method. The 14th Asia Congress of Fluid Mechanics, October 15 - 19, 2013; Hanoi and Halong, Vietnam(In English)

[4]     Shi Yong-qiang, Yang Qing-zhen, Zhou Xin-hai. Application of Harmonic Balance Method to Numerical Model Unsteady Viscous Flow around Oscillating Cascade. Applied Mechanics and Materials Vols.50-51, Part 2, 2011. (EI: 20110813676001) (In English)

[5]     Yongqiang Shi, Qingzhen Yang, Xinhai Zhou. Effect of Aspect Ratio on Flutter Characteristics of Fan/Compressor. The 3rd International Symposium on Jet Propulsion and Power Engineering. September 13-17, 2010. Nanjing, China. (In English)

[6]     Shi Yong-qiang, Yang Qing-zhen, Zhou Xin-hai.  Influence of Blade Thickness on Flutter Characteristics in Fan/Compressor. ACTA AERONAUTICA ET ASTRONAUTICA SINICA. 30(6):979-984, 2009. (EI:20092912195668) (In Chinese)

[7]     Shi Yong-qiang, Wang Quan-qi and Yang Qing-zhen. Analysis of Fluid-Structure Coupling Characteristics in Fan/compressor rotor. Computer Simulation. 28(7):115-119, 2011. (In Chinese)

[8]     Shi Yong-qiang, Yang Qing-zhen. Design of aircraft geometry database and development of database management system. Computer Engineering and Application. 43(36):114-116, 2007. (In Chinese)

[9]     Shi Yong-qiang, Yang Qing-zhen. A study on the data exchange between aircraft geometry database and CAD software. Computer Engineering and Application. 42(22):84-90, 2006. (In Chinese)

[10]  Shi Yong-qiang, Yang Qing-zhen. Design of a experiment simulation platform for aeroengine. GAOXIAO SHIYANSHI GONGZUO YANJIU. 111(4):60-62, 2012. (In Chinese)

[11]  Gao Xiang, Shi Yong-Qiang, Yang Qing-Zhen, Chen Li-Hai. Electromagnetic scattering characteristics of double S-shaped exhaust nozzle with different coating medium parts. Acta Physica Sinica. Accepted. (In Chinese)

[12] Yang Qingzhen, Shi Yongqiang, Huang Xiuquan and Zhou Xinhai. Numerical Analysis of Three-dimensional Unsteady Flow Around Oscillating Cascades. ACTA AERODYNAMICA SINICA. 24(1):62-66, 2006. (EI:06239925705) (In Chinese)

[13]  Yang Qingzhen, Shi Yongqiang, Xiao Jun and Zhou Xinhai. Unsteady Flow Analysis of Oscillating Cascade under Flow/Structure Coupled Condition. Chinese. Journal of Applied Mechanics. 23(2):167-172, 2006. (EI:063210056560) (In Chinese)

[14]  Xiong Jian, Wang Xin-yue, Shi Yong-QiangYan Zi-guang. Aerodynamic optimization design of high bypass ratio separate-flow exhaust system based on parallel multi-objective genetic algorithm.  Journal of Aerospace Power. 27(6):1384-1390, 2012. (EI:20123515381539) (In Chinese)

[15]  Guoxiao, Yang Qingzhen, Shi Yongqiang. Vibration Characteristics Analysis of Wide-chord Hollow Fan Blade. The 2013 International Conference on Structural Engineering, Vibration and Aerospace Engineering. Zhuhai, China, November 23-24, 2013. (In English)

[16] WU Zheng-ke, YANG Qing-zhen and Shi Yong-qiang. Optimization Design of the Dual Throat Fluidic Thrust Vectoring Nozzle based on RBF and PSO. Journal of Propulsion Technology. 2014, has been accepted(In Chinese)

[17]  Wu Zheng-ke, Yang Qing-zhen and Shi Yong-qiang. Particle swarm optimization with particle release and speed limit. Application Research of Computers. 30(3):682-687, 2013. (In Chinese)