Advanced TR-PIV (time-resolved-particle image velocimetry) system was used to measure transient velocity field at a Helmholtz-type valve pulse jet engine exit zone. Test results indicate the cyclical evolution process of velocity field and pressure at the exit zone of valve pulse jet engine
and the maximum time-averaged velocity of the engine is not at the nozzle's exit. The vorticity and duration in the exhaust stage was stronger than that in the inspiratory stage. Measured velocity field shows that transient high-temperature combustion gas does not fully expand at the exit plane
but continues to be expanded at the following exit zone
which is disadvantageous for improving the performance of pulse jet engine.
Numerical study on influence of pre-swirl nozzle radial angles on pre-swirl characteristic
Numerical study of flow characteristics in rotating S-shaped passage with ribs
Theoretical model and experiment of convective heat transfer in microchannel heat sinks
Characteristics of low swirl flow and combustion in a limited space
Effects of secondary injection forms on thrust vector performance of shock vector controlling nozzle
Related Author
毛莎莎
王锁芳
胡伟学
SUN Rui-jia
ZHU Hui-ren
ZHAO Shu
ZHANG Li
WANG Shun-bin
Related Institution
南京航空航天大学 能源与动力学院 航空发动机热环境与热结构工业和信息化部重点实验室
School of Power and Energy,Northwestern Polytechnical University
Turbine Department, China Aviation Powerplant Research Institute, Aviation Industry Corporation of China
Key Laboratory of Enhanced Heat Transfer and Energy Conservation Ministry of Education, College of Environmental and Energy Engineering, Beijing University of Technology
Marine Engineering College, Dalian Maritime University