Research Assistant Professor Department of Mechanics and Aerospace Engineering

Work experience

2010/07 - 2016/12, National University of Singapore, R&D Engineer

2017/01 - 2017/02, Senior Engineer, Wigetworks Ground Effect Aircraft Company, Singapore

2017/03 - 2017/06, Polaris AeroTech Drone Company, CTO + Founder

2017/07 - Today, Assistant Professor of Research, Department of Mechanics and Aerospace Engineering, Southern University of Science and Technology

Learning experience

2006 - 2010, Nanyang Technological University, Department of Aerospace Engineering, Bachelor (First Class)

2012 - 2016, Ph.D., Department of Mechanical Engineering, National University of Singapore.

Honors

2010 EADS TechMaster Scholarship;

2017 Shenzhen High-level Talent Peacock Plan Class C

Personal Profile

Research

Aircraft design, flight stability and control, ground effect aircraft design, flight test


Publications Read More

Papers

1. Wang Hao, Shan Xiaowen, Xu Zhenyu, “A propeller-type vertical take-off and landing fixed-wing aircraft”, a utility model, has been authorized, and the invention has entered the stage of trial. Patent No.: ZL 2017 2 1256895.0.

2. Wang Hao, “A pneumatic vertical take-off and landing aircraft”, utility model patent, utility model, authorized, patent number: ZL 2017 2 0576657.1.

3. Wang Hao, “A multi-stage series cyclone separation device”, utility model, authorized, patent number: ZL 2017 2 0442017.1.

4. Wang Hao, Shan Xiaowen, Xu Zhenyu, Yang Yuan, Meng Lingxiao “A Separated Aircraft for Power System and Control System” utility model, authorized, and the invention entered the stage of trial. Patent No.: ZL 2017 2 1565999.X.

5. Wang Hao, Shan Xiaowen, Li Jianwei, Hu Rui, Yin Yuchen, “A Dual Control System Aircraft”, utility model, authorized, and invention entered the actual trial stage. Patent No.: 201810458136.5.

6. Shan Xiaowen, Wang Hao. “A modular fixed-wing UAV”, a utility model, has been authorized, and the invention has entered the stage of trial. Patent No.: 201810348604.3.

7. Wang Hao, Shan Xiaowen, “A ground effect aircraft”, invention patent. Application No.: 201010882293.9. Application date: 2018-08-03

8. Wang Hao, Shan Xiaowen, “An aircraft based on the height of the rudder control”, invention patent, application number: 201811307693.3. Application date: 2018-11-05

9. Wang, H., Teo, CJ, Khoo, BC, & Goh, CJ (2013). “Computational aerodynamics and flight stability of Wing-In-Ground (WIG) craft”. In Procedia Engineering: 7th Asian-Pacific Conference On Aerospace Technology and Science. (Vol. 67, pp. 15-24). (Keynote Paper)

10. Wang H., CJ Teo, BC Khoo. (2015). "Optimization of aerodynamic performance of a reversed delta wing in ground effect", On 7th Symposium on Applied Aerodynamics and Design of Aerospace Vehicles 2015. (Keynote Paper)

11. Wang H. (2015). "Generalized static stability criterion for Wing-In-Ground (WIG) craft undergoing coupled longitudinal and lateral motion", on 7th Symposium on Applied Aerodynamics And Design of Aerospace Vehicles 2015.

12. Wang H., CJ Teo, BC Khoo, CJ Goh, (2013) "Aerodynamic and stability characteristics of NACA4412 in ground effects", International Journal of Intelligent Unmanned Systems, Vol. 1 Iss: 2, pp.145 - 153.

13. Wang H., CJ Teo, BC Khoo, CJ Goh. (2015). "Stability of the WIG (Wing-In-Ground) effect craft ", on International Symposium on Sustainable aviation 2015.

14. Wang H., CJ Teo, BC Khoo, CJ Goh. (2015). "Effects of viscosity on the aerodynamic performance of a NACA4412 airfoil operating in ground-effect", on 7th Symposium on Applied Aerodynamics and Design of Aerospace Vehicles 2015 .

15. Tiauw Hiong Go, Wang Hao, (2010) "Investigation on propulsion of flapping wing with modified pitch motion", Aircraft Engineering and Aerospace Technology, Vol. 82 Iss: 4, pp.217 – 224

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    2019-11-14
  • SUSTech Annual Research Symposium 2019 comes to a successful close

    2019-11-14
  • Global Scientist Interdisciplinary Forum2020

    2019-10-24

Lab members Read More

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Founded in December 2015, the Department of Mechanics and Aerospace Engineering (MAE) is one of departments in the College of Engineering. It aims to establish a world-leading department in mechanics and aerospace engineering, covering various research areas such as fluid mechanics, aerodynamics, thermodynamics, aeroacoustics, mechanics, combustion, material, and system control. The Department will learn from the best practice of peer departments over the world in order to develop into an international research institution that attends to the national strategic needs in mechanics and aerospace, cultivates outstanding innovative talents, and conducts frontier fundamental research and applied research with social impact. 
The goal of the Department is to become a top-tier international leader through introducing an innovative education system which emphasizes IUR (Industry-University-Research) in close association with the Chinese aerospace industry. The specific objectives are: 1) to nurture innovative talents (learning); 2) to research and develop key technologies (research); and 3) to provide technical services (production) for the national aerospace industry.
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Contact Address

Room408,Block7, chuangyuan

Office Phone

Email

wangh7@sustech.edu.cn

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