Dong Han
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教育工作经历

·           1997/09-1999/06,南京航空航天大学,97级强化班

·           1997/09-2001/06,南京航空航天大学,飞行器设计,学士

·           2001/09-2006/03,南京航空航天大学,飞行器设计,博士,

·           2006/05-2007/04,Utah State University (USA),School of Engineering,Postdoc

·           2007/05-2010/04,Pennsylvania State University (USA),School of Engineering Research Associate

·           2010/09-2016/06,南京航空航天大学,航空宇航学院,副教授

·           2014/12-2015/11,University of Liverpool (UK), School of Engineering,Visiting Scholar

·           2016/06–至今,  南京航空航天大学,航空宇航学院,教授

·           2017/06–至今,  南京航空航天大学,航空宇航学院,博导

研究方向

·           直升机动力学及其控制

·           CFD/CSD/CAE

·           先进旋翼飞行器总体设计

·           智能旋翼飞行器

·           旋翼飞行器多体动力学


代表论著(共计发表论文百余篇,第一作者SCI检索期刊20余篇)

·           Han, D., Yu, W.*, and Roy, S., “A Geometrically Exact Active Beam Theory for Multibody Dynamics Simulation,” Smart Materials and Structures, Vol.16, No. 4, 2007, pp. 1136-1147. 

·           Han, D.* and Smith, E. C, “Lagwise Loads Analysis of a Rotor Blade with an Embedded Chordwise Absorber,” Journal of Aircraft, Vol. 46, No. 4, 2009, pp.1280-1290. 

·           Han, D.*, Wang, H.-W.and Gao, Z., “Aeroelastic Analysis of a Shipboard Helicopter Rotor with Ship Motions during Engagement and Disengagement Operations,” Aerospace Science and Technology, Vol. 16, No. 1, 2012, pp. 1-9.

·           Han, D.*, Wang, J., Smith, E. C. and Lesieutre, G. A., “Transient Loads Control of a Variable Speed Rotor during Resonance Crossing,” AIAA Journal, Vol. 51, No. 1, 2013, pp. 20-29. 

·           Han, D.* and Smith, E. C., “Lagwise Dynamic Analysis of a Variable Speed Rotor,” Aerospace Science and Technology, Vol. 29. No. 1, 2013, pp. 277-286. 

·           Han, D., Pastrikakis, V. and Barakos, G.*, “Helicopter Performance Improvement by Variable Rotor Speed and Variable Blade Twist,” Aerospace Science and Technology, Vol. 54, 2016, pp.164-173. 

·           Han, D.*, “Flap-wise Loads Reduction of Rotor Blades by Embedded Flap-wise Absorbers,” Aeronautical Journal, Vol. 120, No. 1230, 2016, pp.1215-1229.

·           Han, D.*, Pastrikakis, V. and Barakos, G., “Helicopter Performance Improvement by Dynamic Blade Twist,” Aerospace Science and Technology, Vol. 58, 2016, pp. 445-452. 

·           Han, D.* and Barakos, G., “Variable Tail Rotor Speeds for Helicopters with Variable Main Rotor Speeds,” Aeronautical Journal, Vol. 121, No. 1238, 2017, pp. 433-448.

·           Han, D.*, Yang, K., and Barakos, G. N.,“Extendable Chord for Improved Helicopter Rotor Performance,” Aerospace Science and Technology, Vol. 80, 2018, pp. 445-451.

·           Han, D.*, Dong, C, and Barakos, G. N.,“Performance Improvement of Variable Speed Rotors by Gurney Flaps,” Aerospace Science and Technology, Vol. 81, 2018, pp. 118-127.

·           Han, D.*, Yu, L., and Barakos, G. N.,“Transient Aeroelastic Response Control of Shipboard Rotors During Engagements by Gurney Flaps,” Journal of Aircraft, Vol. 56, No.2, 2019, pp. 837-841.

·           Han, D.* and Barakos, G. N., “Rotor Loads Reduction by Dynamically Extendable Chord,” AIAA Journal, Vol. 58, No. 1, 2020, pp. 98-106. 

·           Han, D.* and Barakos, G. N., “Aerodynamic Interference Model for Multi-Rotors in Forward Flight,” Journal of Aircraft, Vol. 57, No. 6, pp. 1220-1223.

·           Han, D.* and Barakos, G. N., “Loads Transfer Principles of a Four-Bladed Scissors Rotor,” Journal of Aircraft, Vol. 59, No.2, 2022, pp. 544-546.

·           Han, D.* and Barakos, G. N., “Transient Aeroelastic Response of a Rotor during Rotor Speed Transition in Forward Flight,” Journal of Aircraft, Vol.59, No. 4, 2022, pp. 1020-1026.

·           Han, D.*, Zhou, L., and Barakos, G. N., “Parametric Investigation of the Flight Performance of a Variable Pitch X-Configuration Quadrotor Aircraft, Journal of Aerospace Engineering, Vol. 35, No. 6, 2022, pp. 04022082.

·           Han, D.* and Barakos, G. N., “Loads Transfer Principles of Coaxial Helicopter Rotors,” Journal of the American Helicopter Society, Vol. 68, No. 1, 2023, pp. 012008.

·           韩东. 《直升机结构动力学》, 科学出版社, 2020.

·           韩东, 万浩云, 张宇杭. 《自适应旋翼性能》, 科学出版社, 2021.

获奖

·           2018年入选第十五批江苏省“六大人才高峰”高层次人才B类

·           2018年获The Royal Aeronautical Society颁发的Written Paper Prizes-Silver Award奖励

·           2019年获中国航空工业集团公司科技进步二等奖

·           2017-2018本科生学风建设工作先进个人

·           2019年入选南京航空航天大学长空学者

·           2018-2019学年校优秀教学二等奖

科研情况

·           主持十四五**预研专用技术、**专项、**领域基金、十三五**预研专用技术、**背景、**背景、国家自然科学基金面上项目、国家自然科学基金青年基金、航空基金、重点实验室基金、六大人才高峰高层次人才等项目

·           参与演示验证、无人机预研、863、探索创新、工信部专项等项目

·           已经授权国家发明专利14项

教学情况

·           目前指导5名博士研究生、12名硕士研究生;毕业19名硕士研究生、3名外国留学生(多人获国家奖学金、优秀硕士毕业生、三好研究生)。

·           主讲课程《直升机结构动力学》、《直升机科技英语》、《旋翼飞行器飞行性能》

·           指导研究生参加科创大赛获国家级二等项一项、三等奖三项、优胜奖一项


  • Educational Experience
  • Work Experience
2003-4 | 2006-3
  • 南京航空航天大学
  • 飞行器设计
  • With Certificate of Graduation for Doctorate Study
  • Doctoral Degree in Engineering

1997-9 | 2001-6
  • 南京航空航天大学
  • 飞行器设计
  • University graduated
  • Bachelor's Degree in Engineering

1994-5 | 1997-7
  • 武汉市第四中学
  • 普通高中毕业
  • 无学位

  • Social Affiliations
  • Research Focus
Personal Information

Professor
Supervisor of Doctorate Candidates

Gender:Male

Alma Mater:南京航空航天大学

Education Level:南京航空航天大学

Degree:Doctoral Degree in Engineering

School/Department:College of Aerospace Engineering

Discipline:Flight Vehicle Design

Business Address:A5-311

Contact Information:025-84896444 donghan@nuaa.edu.cn

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