Affiliation:
1. Department of Aerospace Science and Technology, Space Engineering University , Beijing 101416, China
Abstract
Based on steady-state experiments, a three-dimensional (3D) simulation study under pulsation conditions was carried out. This was performed to study the effect of pulsation of the supply system on the atomization characteristics of a gas-centered swirl coaxial injector. The results indicated that the spray shape resembled a pagoda when the Klystron effect occurred. When the low-frequency pulsation (200 Hz) was applied to the liquid inlet, the peak of the exit pressure was close to the trough of the inlet mass flow rate. Meanwhile, the exit mass flow rate and pressure were approximately sinusoidal. There was no significant lag effect in the response of the exit mass flow rate to the inlet mass flow rate but with a small sawtooth-like oscillation. Increasing the amplitude of the liquid inlet disturbance amplified the exit mass flow rate fluctuation, which was greater than the set amplitude of the inlet pulsation. The dominant frequency of the injector exit mass flow rate and pressure variation was significantly less than the inlet pulsation frequency when the frequency of the liquid inlet pulsation was increased to 1000 Hz. This was due to the low-pass filtering effect of the annular slit. There was no significant change in the overall spray morphology for the gas inlet pulsation. By applying the same amplitude and frequency of pulsation to the gas and liquid inlets of the injector, the pulsation of the liquid inlet had a stronger effect on the injector exit spray than that of the gas inlet.
Funder
National Natural Science Foundation of China
Subject
General Physics and Astronomy
Reference40 articles.
1. Effect of baffle injectors on the first-order tangential acoustic mode in a cylindrical combustor;Chin. J. Aeronaut.,2022
2. Comparative study of spray characteristics of gas-centered and liquid-centered swirl coaxial injectors;J. Propul. Power,2010
3. Z.
Kang
, “The unsteady atomization mechanism and combustion characteristics of gas-iiquid swirl coaxial,” Ph.D. thesis, National University of Defense Technology, Changsha, 2016.
4. Liquid-propellant rocket engine injector dynamics;J. Propul. Power,1998