In order to seek the effective injector type of the power-law non-Newtonian propellant
a water-based simulants whose rheological behavior was in accord with actual propellant was used. The injectors
including plain orifice
impinging injector
shearing impinging pneumatic atomizer
effervescent atomizer and swirling injector were investigated by experiments
and the effects of different injectors and their structural parameters on the spray characteristics were compared. The results indicate that the impinging injector is effective and its impinging angle and injection velocity are the main influencing parameters to spray property. The effervescent atomizer is an effective injector type. Water-based simulants break up and produce drops when ratio of air/liquid mass flow rate is about 4%.
Effects of throttling level on spray characteristics of gas⁃liquid pintle injector unit
Thermal friction characteristics analysis of helical gears under non-Newtonian fluid and big slide-roll ratio
Impact effect of liquid rocket motor exhaust plume on launching platform
Vaporization and spray characteristics of vaporizer
Experiment on spray characteristics of periodic air-assist direct injection atomizer
Related Author
Ping LI
Anlong YANG
Baoe YANG
Botao ZHANG
杨剑飞
顾俊杰
朱如鹏
陆凤霞
Related Institution
National Key Laboratory of Science and Technology on Liquid Rocket Engines,Xi'an Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
Academy of Aerospace Propulsion Technology,China Aerospace Science and Technology Corporation
南京航空航天大学 机电学院
Department of Aerospace Equipment, The Academy of Equipment
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics