supported by the National Natural Science Foundation of China(Nos.51522606,51507187,51276197,51407197,and 11472306)
We conducted experiments in a wind tunnel with Mach number 2 to explore the evolution of a transverse plasma jet and its modification effect on a shock wave induced by a ramp with an angle of 24°. The transverse plas...
supported by the National Natural Science Foundation of China(Grant Nos.11472306,51276197,and 51336011)
Electrical characteristics and optical emission spectrum of the radio frequency (RF) surface dielectric barrier discharge (SDBD) plasma actuation are investigated experimentally in this paper. Influences of operat...
Project supported by the National Natural Science Foundation of China(Grant Nos.61503302,51207169,and 51276197);the China Postdoctoral Science Foundation(Grant No.2014M562446);the Natural Science Foundation of Shaanxi Province,China(Grant No.2015JM1001)
Plasma flow control(PFC) is a new kind of active flow control technology, which can improve the aerodynamic performances of aircrafts remarkably. The flow separation control of an unmanned air vehicle(UAV) by nano...
supported by the Key Program of the National Natural Science Foundation of China(Grant No.51336011);the National Natural Science Foundationof China(Grant Nos.51207169 and 51276197)
The potential of controlling shockwave-boundary layer interactions (SWBLIs) in air by plasma aerodynamic actua- tion is demonstrated. Experiments are conducted in a Mach 3 in-draft air tunnel. The separation-inducin...