Dr. Yang Zhang
Email：yangzhang@ujs.edu.cn
Add：Institute for Energy Research, Jiangsu University
Research Interests
Atomization and combustion process of kerosene rocket engine
Numerical simulation theory of internal flow field in rocket engine of combined power aircraft
Projects
1. Research of soot test technology and test verification of gas generator，in research;
2. Study on mixing and combustion characteristics of pintle injector，in research;
3. Study on GO2/RP-3 rocket system of combined power aircraft, 2017-2019;
4. Study on experimental system of LO2/RP-3 chamber, 2015-2016.
Selected papers
1. Yang Zhang, Nanjia Yu, Hui Tian, et al. Experimental and Numerical Investigations on Flow Field Characteristics of Pintle Injector [J]. Aerospace Science and Technology, Volume 103, August 2020, 105924.
2. Yang Zhang, Nanjia Yu, Quan Quan, et al. Investigations of variable thrust liquid oxygen/kerosene engine using a pintle injector [C]. Proceedings of the 69th International Astronautical Congress: IAC 2018.
3. Nanjia Yu, Yang Zhang, Feng Li, et al. Numerical and experimental investigations of single-element and double-element injectors using gaseous oxygen/gaseous methane [J]. Aerospace Science and Technology, 2018, 75(24-34).
4. Jian Dai, Guobiao Cai, Yang Zhang, et al. Experimental and numerical investigation of combustion characteristics on GO2/GH2 shear coaxial injector [J]. Aerospace Science and Technology, 2018, 77(725-32).
5. Guobiao Cai, Jian Dai, Yang Zhang, et al. Combustion behaviors of GO2/GH2 swirl-coaxial injector using non-intrusive optical diagnostics [J]. Acta Astronautica, 2016, 123(246–56).
6. Jian Dai, Guobiao Cai, Yang Zhang, et al. Experimental investigations of coaxial injectors in a laboratory-scale rocket combustor [J]. Aerospace Science and Technology, 2016, 59(41-51).
7. Nanjia Yu, Qilin Bao, Feng Li, Yang Zhang*. Experiment on coaxial shear injector of GO2/GCH4 based on PLIF [J]. Journal of Aerospace Power, 2018, 33(10):188-196.
Patents
Nanjia Yu；Yang Zhang；Jian Dai；Feng Li. Rectangular transparent combustion chamber for optical diagnosis of small rocket engine，patent number：ZL201610284580.0
