zhang ke shi


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

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The basic information

zhang ke shi

School of Aeronautics

Postgraduate

Doctor

Associate Professor

Work Experience

2008- , Associate professor, School of Aeronautics, Northwestern Polytechnical University

2008-2010 , Visit scholar, School of Aeronautics, Northwestern Polytechnical University

2006-2008, Postdoctor, School of Aeronautics, Northwestern Polytechnical University

2002-2006 , PhD student, School of Aeronautics, Northwestern Polytechnical University

2000-2003 , Graduate student, School of Aeronautics, Northwestern Polytechnical University

1996-2000 , Undergraduate student, School of Aeronautics, Northwestern Polytechnical University

Education And Teaching

1. "Aircraft Conceptual Design", undergraduate student course for the international school students, 40 hours.

2. "Multidisciplinary Design Optimization of Aircraft Engineering", graduate student course, 40 hours. 

Admission Information

Research interests:

1. Multidisciplinary design optimization of Aircraft: theory and methods, such as bilevel optimization, surrogate modeling optimization, robust optimization.

2. Application of multidisciplinary design optimization in the novel concepts of large transport aircraft, such as truss-braced wing aircraft, laminar flow aircraft.

3. Multidisciplinary design optimization of wings. 

Scientific Research

Main Projects (PI and Co-PI):

1. Development of New Cokriging-based Method for Hi-dimensional Aerodynamic Optimization, supported by National Natural Science Foundation of China, 2013-2016.

2. Development of New Bilevel optimization Framework for Aircraft Multidisciplinary and Multiobjective Optimization, supported by National Natural Science Foundation of China, 2008-2010.

3. Investigation of Design and Experiment Technologies of Windmill Airfoil Family, supported by Ministry of Science and Technology 863, 2012-2015.

4. Investigation of Commercial Hybrid Airship Technologies for Large Cargo Transport, supported by Ministry of Science and Technology 863, 2007-2008.

5. Development of Multidisciplinary Multiobjective Optimization Method for Aircraft Conceptual Design, supported by Ph.D Programs Foundation of Ministry of Education of China, 2008-2010.

6. Investigation of Bilevel Optimization Method for Aircraft Multidisciplinary Multiobjective Design, supported by China Postdoctoral Science Foundation (the First Prize), 2007-2008.

7. Investigation of Noise Controlling of Propeller, supported by AVIC Aerodynamics Research Institute, 2013-2014.

Representative Papers:

[1] Ke-shi Zhang, "Concurrent Subspace Optimization for Aircraft System Design," Aeronautics and Astronautics, Intech, ISBN 978-953-307-473-3, 2011.

[2] Zhang, K.S., Bakar, A., Ji, P.B., Han, Z.H. and Li, X.P., "Multidisciplinary Optimization of Truss-Braced Wing Layout," 29th Congress of the International Council of the Aeronautical Sciences, St. Petersburg, Russia, Sep.7-12, 2014.(EI)

[3] Zhang, K.S. and Han, Z.H., "Support Vector Regressio-based Multidisciplinary Design Optimization in Aircraft Conceptual Design," 47th AIAA Aerospace Sciences Meeting and Exhibit, Grapvine, Dallas, Jan.9-12, 2013.(EI)

[4] Zhang, K.S., Ji, P.B. and Bakar, A., "Multidisciplinary Evaluation of Truss-Braced Wing for Future Green Aircraft," 28th Congress of the International Council of the Aeronautical Sciences, Brisbane, Australia, Sep.23-28, 2012.(EI)

[5] Zhang, K.S., Han, Z.H., Song, B.F., "Flight Performance Analysis of Hybrid Airship: Revised Analytical Formulation," Journal of Aircraft, 2010, 47(4):1318-1330. (SCI, EI)

[6] Zhang, K.S., Li, W.J. and Song, W.P., "Development of Concurrent Subspace Optimization Method and Its Application in Parallel Design of Complex System," Journal of Basic Science and Engineering, 2009, 17(1): 92-104. (EI)

[7] Zhang, K.S., Han, Z.H., Li, W.J. and Song, W.P., "Bilevel Adaptive Weighted Sum Method for Multidisciplinary Multi-Objective Optimization," AIAA Journal, 2008, 46(10): 2611-2622. (SCI, EI)

[8] Zhang, K.S., Han, Z.H., Li, W.J. and Song, W.P., "Coupled Aerodynamic/Structural Optimization of a Subsonic Transport Wing Using a Surrogate Model," Journal of Aircraft, 2008, 45(6): 2167-2171. (SCI, EI)

[9] Zhang, K.S., Han, Z.H., Li, W.J. and Song, W.P.,  "A Method of Coupled Aerodynamic/Structural Integration Optimization for Transport-wing Design," Acta Aerodynamica Sinica, 2008, 26(1): 1-7.(EI)

[10] Zhang, K.S. and Li, W.J., "Improving GSECSSO Algorithm and Applying It to Aircraft Conceptual Design," Journal of Northwestern Polytechnical University, 2008, 26(1): 110-115.(EI)

[11] Zhang, K.S., Han, Z.H., Li, W.J. and Li, X.,  "Multidisciplinary Aerodynamic/Structural Design Optimization for High Subsonic Transport Wing Using Approximation Technique," Acta Aeronautica Sinica, 2006, 27(5): 810-815. (EI) 

[12] Zhang, K.S., Li, W.J. and Wei, H.Y., "A New Method for Optimum Allocation of Design Requirements in Aircraft Conceptual Design," Chinese Journal of Aeronautics, 2006, 19(3): 203-211.(EI)