han zhong hua


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

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The basic information

han zhong hua

School of Aeronautics

Postgraduate

Doctor

Professor

Work Experience

Feb.2015-now

Professor, associate head of Department of Fluid Mechanics, School of Aeronautics, NPU (exceptional promotion for outstanding youth scholar)

Mainly researching on the topic “efficient surrogate-based optimization with applications to aircraft aerodynamic design and multidisciplinary design optimization (MDO)”.

Feb.2014-Jan.2015

Research scientist, Institute of Aerodynamics and Flow Technology, Germany Aerospace Center (DLR)

work with “aerodynamic surrogate models” group and "MDO" group about the topic “efficient surrogate modeling and aerodynamic optimization of forward-swept wing configuration”

Aug.2013-Sep.2013

Visiting professor, Institute of Aerodynamics and Flow Technology, Germany Aerospace Center (DLR)

Collaborative research work with “aerodynamic surrogate models” group and "MDO" group about the topic “multidisciplinary design optimization using surrogate models: architecture and applications to aircraft”

May. 2013-Jan.2014

Professor, Department of Fluid Mechanics, School of Aeronautics, NPU (exceptional promotion for outstanding youth scholar)

Mainly researching on the topic “efficient surrogate-based optimization with applications to aircraft aerodynamic design and multidisciplinary design optimization (MDO)”.

Nov. 2011-Jan.2014

Dean assistant, School of Aeronautics, head of School Internationalization Office

Teaching admistration of English courses for international education; international cooperation and exchange.

Sep.2010-Apr. 2013

Associate professor, Department of Fluid Mechanics, School of Aeronautics, NPU

Mainly researched on “efficient surrogate-based optimization with applications to aircraft aerodynamic design”.

Oct.2007-Aug.2010 AAug.2010

Research scientist, Center for Computer Applications in AeroSpace Engineering (C2A2S2E), Institute of Aerodynamics and Flow Technology, Germany Aerospace Center (DLR)

Mainly researched on the topic “surrogate modeling and variable-fidelity modeling methods in the context of aerodynamic data for loads and optimization”.

Mar.2002-Sep.2007

Ph.D candidates, faculty in Department of Aircraft Design Engineering, NPU

Mainly researched on “efficient numerical simulation method for complex, unsteady flows past wing/helicopter rotors and active flow control via zero-mass-flux synthetic jet”

Apr.2000-Apr. 2003

B.S. and M.S. student, NPU

Researched on numerical simulation of inviscid flows past helicopter rotor in hover and forward flight as well as aeroacoustic noise prediction using Kirchhoff and Ffowcs-Williams Hawkings methods

Education Experience

Mar.2002-Jul.2007

Ph.D, fluid dynamics, Northwestern Polytechnical University

Sep.2000-Mar.2003

M.S., fluid dynamics, Northwestern Polytechnical University

Sep.1996-Jul.2000

B.S., aerodynamics and flight mechanics, Northwestern Polytechnical University


Education And Teaching

Teaching Activities (2010-2015)

l             “Fundamental of aerodynamics”, undergraduate student course (in Chinese)

l             “High-speed aerodynamics”, undergraduate student course (in Chinese)

l           “Aerodynamic design optimization”, ,graduate student course (in Chinese)

l             “Aircraft aerodynamic estimation and flight performance calculation”, undergraduate student projects (in Chinese)

l             “Rotorcraft aerodynamics”, graduate student course (in Chinese)

l           “Computational fluid dynamics”, English course for international mixed class graduate students (In English)

Awards Information

Sep. 2013, Grand prize of “Wu Ya-Jun award for outstanding youth scholar in NPU”

Jun. 2013, “NPU award for excellent undergraduate thesis supervisor”

Dec. 2012, “Undergraduate teaching award in School of Aeronautics

Dec.2012, “Outstand youth scholar award in School of Aeronautics

Jun. 2012, “NPU award for excellent undergraduate thesis supervisor”

Dec.2011, “Undergraduate teaching award in School of Aeronautics

May. 2011 “NPU new-generation youth scholar award for innovative research directions”

Apr. 2010, “NPU Aoxiang-star award”

Scientific Research

ResearchGate link

<a href="https://www.researchgate.net/profile/Zhong_Hua_Han">Zhong-Hua Han on ResearchGate</a> 

Research Interests

My research interests are in the areas of aircraft aerodynamic design and related topics

lAerodynamic data : surrogate modeling of aircraft aerodynamic data

lAerodynamic opt. & engineering design methodologies: efficient surrogate-based optimization

lAerodynamic design : aircraft airfoil/wing aerodynamic design

lNovel aerodynamic configuration : forward-swept natural-laminar-flow (NLF) wing

llMDO : multidisciplinary design optimization

List of Selected Research Projects

Project name (translated)

From

Funding

Duration

PI

A New Optimization Method for High-Dimensional Aerodynamic Design Problems Based on an Improved Co-Kriging Model

National Natural Science Foundation of China

800,000 RMB

2013-2016

Zhong-Hua Han

Design and Experiment of Airfoil Family for Large-Size Wind Turbines

“863” Program for New-Type Energy

6,830,000 RMB

2012-2015

Wen-Ping Song & Zhong-Hua Han

An Cokriging Model for Surrogate Modeling of High-Dimensional Aerodynamic Data

National Natural Science Foundation of China

250,000

RMB

2010-2012

Zhong-Hua Han

An Novel Aerodynamic Optimization Method Based on Gradient-Enhanced Kriging

Aeronautical Science Foundation of China

100,000

RMB

2011-2013

Zhong-Hua Han

A High-Fidelity Computational Aerodynamic Method for Natural-Laminar-Flow Wing and Efficient Optimization Method

National Aerodynamic Pre-Research Foundation

700,000

RMB

2011-2015

Wen-Ping Song & Zhong-Hua Han

An Optimization Design Method for Reducing the Aeroacoustic Noise of Propeller

AVIC Aerodynamics Research Institute

270,000

RMB

2012-2014

Zhong-Hua Han

Surrogate Modeling Methods Towards Optimum Design of the High-Lift Aerodynamic Devices of C919 Aircraft

Commercial Aircraft Corporation of China (COMAC)

180,000

RMB

2011-2012

Zhong-Hua Han

Simulation of the Flow Around High-spped Configurations and Optimization

Chinese Aerospace Science & Industry Corporation

700,000

RMB

2012-2012

Wen-Ping Song & Zhong-Hua Han

Exploration Study of Novel Laminar Wing for Future Aircraft

NPU Program for Youth Scholar

400,000

RMB

2011-2013

Zhong-Hua Han

New Surrogate Models for High-Dimensional Aerodynamic Data

NPU Aoxiang-Star Program for Youth Scholar

60,000

RMB

2010-2013

Zhong-Hua Han

List of Publications (Dr. Zhong-Hua Han)

Book Chapters

1.G?rtz, S., Zimmermann, R., Han, Z. -H., ”Variable-Fidelity and Reduced-Order Models for Aero Data for Loads Predictions,” N. Kroll, et al. (eds.) Computational Flight Testing, Notes on Numerical Fluid Mechanics and Multidisciplinary Design,, pp.99-112.

3.Han, Z. -H., G?rtz, S., and Hain, R., "A Variable-Fidelity Modeling Method for Aero-Loads Prediction," A. Dillmann, G. Heller, M. Klaas, H.-P. Kreplin, W. Nitsche, W. Schr?der (Eds.), "New Results in Numerical and Experimental Fluid Mechanics VII", Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 112, Springer, 2010, pp. 17-25.

Journal Publications

. -H., G?rtz, S., and Zimmermann, R., “Improving Variable-Fidelity Surrogate Modeling via Gradient-Enhanced Kriging and a Generalized Hybrid Bridge Function,” Aerospace Science and Technology, Vol. 25, No. 1, 2013, pp. 177-189 doi:10.1016/j.ast.2012.01.006

2.Advances in Aeronautical Science and Engineering, Vol. 4. No. 1, 2013, pp.97-105 (In Chinese)

3.

4.Han, Z. -H., Zhang, K. -S., Song, W. -P., and Qiao, Z. -D., “Optimization of Active Flow Control over an Airfoil Using a Surrogate-Management Framework,” Journal of Aircraft, Vol. 47, No. 2, 2010, pp. 603-612. doi: 10.2514/1.45899

7.Journal of Northwestern Polytechnical University, Vol. 30, No. 6, 2012, pp. 830-835. (in Chinese)

8.ACTA Aeronautica Sinica, Vol. 29, No. 1, 2011, pp.97-101. (in Chinese) doi: 10.3969/j.issn.0258-1825.2011.01.016

9.Acta Aeronautica ET Astronautica Sinica, Vol. 32, No. 12, 2011, pp. 2204-2212 (doi: 11-1929/V.20110906.1123.002)

10.Acta Energiae Solaris Sinica, Vol. 32, No. 1, 2010, pp. 91-95. (in Chinese)

11.Journal of Northwestern Polytechnical University, Vol. 29, No. 4, 2010, pp. 503-510. (in Chinese) doi: 10.3969/j.issn.1000-2758.2010.04.006

12.Song, W. -P., Yu, L., and Han, Z. -H., “Status of Investigation on Airframe Noise Computation,” Advances in Aeronautical Science and Engineering, Vol. 1, No. 2, 2010, pp. 125-131. (in Chinese) doi: 0.3969/j.issn.1674-8190.2010.02.007

14.Xie, F. -T., Song, W. -P., and Han, Z. -H., “Numerical Study of High-Resolution Scheme Based on Preconditioning Method,” Journal of Aircraft, Vol. 46, No. 2, 2009, pp. 520-525. doi: 10.2514/1.37976

17.ACTA Aerodynamica Sinica, Vol. 27, No. 6, 2009, pp. 639-644. (in Chinese) doi: 10.3969/j.issn.0258-1825.2009.06.003

18.10.3969/j.issn.1001-246X.2009.06.007

19.10.3969/j.issn.1001-246X.2009.05.005

Journal of Northwestern Polytechnical University, Vol. 27, No. 2, 2009, pp. 151-156. (in Chinese) doi: 0.3969/j.issn.1000-2758.2009.02.002

21.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, Vol. 46 No. 10, 2008, pp. 2611-2622. doi: 10.2514/1.36853

23.ACTA Aerodynamica Sinica, Vol. 26. No. 1, 2008, pp.1-7. (in Chinese) doi: 10.3969/j.issn.0258-1825.2008.01.001

24.ACTA Aeronautica ET Astronautica Sinica, Vol. 29, No. 3, 2008, pp. 583-595. (in Chinese)

25.Han, Z. -H., Qiao, Z. -D., and Song, W. -P., “Numerical Simulation of Active Flow Control to Airfoil Stall Using Local Synthetic Jet,” ACTA Aeronautica ET Astronautica Sinica, Vol. 28, No. 5, 2007, pp. 1040-1046. (in Chinese)

27.Prediction of Hovering Rotor Noise Based on Reynolds-Averaged Navier-Stokes Simulation,” Journal of Aircraft, Vol. 44, No. 4,2007, pp. 1391-1395. doi: 10.2514/1.28310

28.10.3969/j.issn.0258-1825.2007.01.006.

29.Aerodynamic Characteristics of Flapping Airfoils at Low Reynolds Number,” ACTA Aerodynamica Sinica, Vol. 25, No. 1, 2007, pp. 104-109. (in Chinese) doi: 10.3969/j.issn.0258-1825.2007.01.019

30.Xie, F. -T., Han, Z. -H., and Song, W. -P., “The Analysis of the Directivity of Helicopter Rotor Noise Based on a New Acoustic Method,” Helicopter Technique, No. 1, 2007, pp. 11-15. (In Chinese) doi: 10.3969/j.issn.1673-1220.2007.01.003

32.Han, Z. -H., Qiao, Z. -D, Xiong, J. -T., and He, G. -H., “Development of an Efficient Viscous Preconditioning Method and Its Application to Numerical Simulation of Flows over Airfoils,” Journal of Northwestern Polytechnical University, Vol. 24, No. 3, 2006. pp. 275-279. (in Chinese) doi: 10.3969/j.issn.1000-2758.2006.03.001

34.Xiong, J. -T., Qiao, Z. -D., and Han, Z. -H., “Optimum Aerodynamic Design of Transonic Wing Based on Response Surface Methodology,” ACTA Aeronautica ET Astronautica Sinica, Vol. 27, No.3, 2006, pp. 399-402. (in Chinese)

36.ournal of Northwestern Polytechnical University, Vol. 24, No. 2, 2006, pp. 232-236. (in Chinese) doi: 10.3969/j.issn.1000-2758.2006.02.022

37.10.3969/j.issn.1001-3997.2006.08.062

38.10.3969/j.issn.0258-1825.2004.01.009

39.Han, Z. -H., Song, W. -P., and Qiao, Z. -D., “On Improving HSI Noise Prediction for Helicopter Rotor in Forward Flight When Flow Field is Partially near Sonic Speed,” Journal of Northwestern Polytechnical University, Vol. 21, No. 1, 2003, pp. 95-98. (in Chinese) doi: 10.3969/j.issn.1000-2758.2003.01.024

41.Song, W. -P., Han, Z. -H., Yang, A. -M., and Qiao, Z. -D., “A High Efficiency Method for Calculating the Aeroacoustic Noise of Transonic Rotors,” Journal of Northwestern Polytechnical University, Vol. 19, No. 4, 2001, pp. 515-520. (In Chinese) doi: 10.3969/j.issn.1000-2758.2001.04.006

43.10.3969/j.issn.1001-246X.2001.06.017

International Conference Papers

1.Han, Z. -H., Liu, J., Song, W. -P., and Zhang, K. -S., “Surrogate-based Aerodynamic Shape Optimization with Application to Wind Turbine Airfoils,” AIAA paper 2013-1108, Jan. 7-10, Grapevine, Texas, 2013.

2.Zhang, K. -S., Han Z. -H., “Support Vector Regression-based multidisciplinary Design Optimization in Aircraft Conceptual Design,” AIAA paper 2013-1160, Jan. 7-10, Grapevine, Texas, 2013.

3.Han, Z. -H., “Improving Adjoint-based Aerodynamic Optimization via Gradient-Enhanced Kriging,” AIAA paper 2012-0670, Jan. 4-7, Nashville, Tennessee, 2012.

4.Liu, J., Han, Z. -H., and Song, W. -P., “Efficient Kriging-Based Aerodynamic Design of Transonic Airfoils: Some Key Issues,” AIAA paper 2012-0967, Jan. 4-7, Nashville, Tennessee, 2012.

5.Han, Z. -H., Deng, J., Liu, J., Zhang, K. -S., and Song, W. -P., “Design of Laminar Supercritical Airfoils Based on Navier-Stokes Equations,” 28th Congress of International Council of the Aeronautical Sciences, 23 - 28 September, Brisbane, Australia, 2012,Paper ICAS 2012-2.2.2

6.Liu, J., Han, Z. -H., and Song, W. -P., “Comparison of Infill Sampling Criteria in Kriging-Based Aerodynamic Optimization,” 28th Congress of the International Council of the Aeronautical Sciences 2012, 23 - 28 September , Brisbane, Australia, 2012, Paper ICAS2012-11.10ST

7.Zhang, K. -S., Ji, P. -B., Bakar, A., and Han, Z. -H., “Multidisciplinary Evaluation of Truss-Braced Wing for Future Green Aircraft,” 28th Congress of the International Council of the Aeronautical Sciences 2012, 23 - 28 September, Brisbane, Australia, 2012, ICAS 2012,v1,pp. 580-587.

8.Han, Z. -H., Zimmermann, R., and G?rtz, S., "A New Cokriging Method for Variable-Fidelity Surrogate Modeling of Aerodynamic Data ," AIAA Paper 2010-1225 , Jan. 4-7, Orlando, Florida, 2010

9.Han, Z. -H., Zhang, K. -S., “Towards High-Dimensional Aerodynamic Shape Optimization: Surrogate Modeling via Gradient-Enhanced Kriging”, Proceed of 2010 Asia-Pacific International Symposium on Aerospace Technology, 13-15 September, Xi’an, China,2010, Vol. 1 and Vol. 2, 2010, pp. 19-22,

10.Han, Z. -H., Zhang, K. -S., “An Analytical Comparison of Kriging and Radial Basis Functions for Surrogate Modeling,” S. Chellappan et al. (Eds.): Proceeding of the 2010 IRAST International Congress on Computer Applications and Computational Science, CACS 2010 4-6 Dec. 2010, Singapore, pp.162-166.

11.Song W. -P., Xu R. -F., and Han Z. -H., “Study on the improved Kriging-based optimization method for aerodynamic design,” 27th Congress of the International Council of the Aeronautical Sciences 2010, Nice, France, Sep. 2010.

12.Han, Z. -H., Zhang, K. -S., Song, W. -P., and Qiao, Z. -D., “Optimization of Active Flow Control over an Airfoil Using Surrogate Management Framework,” AIAA paper 2009-1280, Jan. 5-8, Orlando, Florida, 2009.

13.Han, Z. -H., Song, W. -P., and Qiao, Z. -D., “On Limitations of Active Stall Control Over a High-Lift Airfoil Using Synthetic Jet Technology,” AIAA paper 2009-534, Jan. 5-8,Orlando, Florida, 2009

14.Han, Z.-H., G?rtz, S., and Zimmermann, R., “On Improving Efficiency and Accuracy of Variable-Fidelity Surrogate Modeling in Aero-data for Loads Context,” Proceeding of CEAS 2009 European Air and Space Conference, Oct. 26-29, Manchester, UK, 2009

15.Dwight, R. and Han, Z. -H., “Efficient Uncertainty Quantification Using Gradient-Enhanced Kriging,” AIAA paper 2009-2276, May 4-7, Palm Springs, California, 2009.

16.Zhang, K. -S., Han, Z. -H, and Song, B. -F, “Flight Performance Analysis of Hybrid Airship, ” AIAA paper 2009-901 , Jan. 5-8,Orlando, Florida, 2009

17.Han, Z. -H., G?rtz, S., and Hain, R., “A Variable-Fidelity Modeling Method for Aero-Loads Prediction,” Proceedings AG STAB Symposium 2008, 3. - 4. Nov., RWTH Aachen, Germany, 2008

18.Han, Z. -H., Zhang, K. -S., Song, W. -P., and Qiao, Z. -D. “Computational Aeroacoustic Noise Prediction for Helicopter Rotor in Forward Flight, ” AIAA paper 2008-46, Jan. 7-10,Reno, Nevada, 2008

19.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,” AIAA paper 2008-897, Jan.7-10, Reno, Nevada, 2008.

20.Zhang, K. -S., Han, Z. -H., Li, W. -J. and Song, W. -P., “Bi-level Adaptive Weighted Sum Method for Multidisciplinary Multi-objective Optimization,” AIAA paper 2008-908, Jan.7-10, Reno, Nevada, 2008.

21.Xie, F. -T., Song, W. -P., and Han, Z. -H., “Numerical Study of High-Resolution Scheme Based on Preconditioning Method,” AIAA paper 2008-0695, January 7- 10, Reno, NV, 2008.

22.Han, Z. -H., He, F., Song, W. -P., and Qiao, Z. -D. “A Preconditioned Multigrid Method for Efficient Simulation of Three-Dimensional Compressible and Incompressible Flows over Wing and Wing-Body Configuration,” Joint Russia-China Aerospace conference, April Xi’an, 2006.

23.Xie, F. -T., Han, Z. -H., and Song, W. -P., “The Analysis of the Directivity of Helicopter Rotor Noise Based on a New Computational Prediction Method,” Joint Russia-China Aerospace Conference, April, Xi’an, 2006.

24.Han Z. -H., Qiao Z. -D., Song W. -P., and Xiong, J. -T., “An Efficient Preconditioning Method and Its application to Numerical Simulation of Steady and Unsteady Viscous Flows,” 28th Congress of the International Council of the Aeronautical Sciences 2006, Sep, 3-8, Hamburg, Germany, 2006.

25.Song, W. -P., Han, Z. -H., and Qiao, Z. -D., “Computational Aeroacoustic Prediction of Transonic Rotor Noise Based on Reynolds-Averaged Navier-Stokes Flow Simulation,” 25th Congress of the International Council of the Aeronautical Sciences 2006, Sep, 3-8, Hamburg, Germany, 2006.

26.Xiong, J. -T., Qiao, Z. -D., and Han, Z. -H., “Aerodynamic shape optimization of transonic airfoil and wing using response surface methodology,” 25th Congress of the International Council of the Aeronautical Sciences 2006, Sep, 3-8, Hamburg, Germany, 2006.

27.Han, Z. -H., Song, W. -P., and Qiao Z. -D., “Investigation of Rotor Noise Prediction Using Different Aeroacoustic Methods in time domain,” 24th Congress of the International Council of the Aeronautical Sciences 2004, Aug.29-Sep.3, Yogohama, Japan, 2004.

Social Appointments

1、Associate editor of international journal "The Scientific World Journal"
2、member AIAA, member Chinese Society of Aerodynamics