Faculty

WANG Hao
Research Assistant Professor
wangh7@sustc.edu.cn

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;

 

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