Xi'an
China
Air Force Engineering University
RDC, Tesla valve, pressure feedback, mode control, pressure gain
Two-phase RDE, Heat release, Performence, Structural parameters, Incoming-flow parameters
Supersonic cavity flow, Plasma actuation, flow control, instability
Spiral-tubular discharge, DBD, Ozone, Reaction pathway analysis, Water
Supersonic cavity flow, Plasma actuation, flow control, Shear layer, K-H instability
coated pipe, chill-down, temperature gradient, re-wetting, Performance optimization
Rotating detonation engine, Bypass channel, Convergent nozzle, Total pressure gain, Combustion efficiency
Thermoacoustic instability, Limit cycle, Floquet exponent
Ignition, Scramjet Engine, Supersonic combustion, High-energy spark