CHina
Space Engineering University
Rocket engine, transverse combustion instability, stress-blended eddy simulation, self-excited, dynamic mode decomposition, driving mechanism
Nonlinear dynamics, Thermoacoustic instability, Bifurcation, Swirl flame
Preheated kerosene Injector arrangementsSspray performanceNumerical investigation
Rib area portion, PEM fuel cell, Distribution, Electric resistance, performance
Nuclear thermal rocket engine, Fuel element, Coolant channel, Uniformity, Flow heat transfer
Liquid transverse jetPreheat temperaturesSpray and flow field structures
Injection temperature Back pressureSpray characteristicNumerical investigation