Single pulse combustion test of high-frequency instability of rocket engine

Acta Astronautica - Tập 178 - Trang 110-116 - 2021
Ryoya Umeoka1, Yuuki Mishina1, Takeshi Kanda2
1Department of Mechanical Engineering, Chubu University, Kasugai, Aichi 487-8501, Japan
2Department of Astronautics and Aeronautics, Chubu University, Kasugai, Aichi, 487-8501, Japan

Tài liệu tham khảo

Sutton, 1986, vol. 134, 184 Chehroudi, 2010, vol. 2 1972 Oefelein, 1993, Comprehensive review of liquid-propellant combustion instability in F-1 engines, J. Propul. Power, 9, 657, 10.2514/3.23674 Culick, 1995 Crocco, 1962, Transverse combustion instability in liquid propellant rocket motors, ARS J., 32, 366, 10.2514/8.6022 Betelin, 2012, Evaporation and ignition of droplets in combustion chambers modeling and simulatiom, Acta Astronaut., 70, 23, 10.1016/j.actaastro.2011.06.021 Sirignano, 1995 Meng, 2014, Vaporization of two liquid oxygen (LOX) droplets in tandem in convective hydrogen streams at supercritical pressures, Int. J. Heat Mass Tran., 68, 500, 10.1016/j.ijheatmasstransfer.2013.09.041 Xu, 2018, A physics-based approach to modeling real-fuel combustion chemistry – II. Reaction kinetics models of jet and rocket fuels, Combust. Flame, 193, 520, 10.1016/j.combustflame.2018.03.021 Armbruster, 2020, Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines, Acta Astronaut., 169, 170, 10.1016/j.actaastro.2019.11.040 Wanbainen, 1967 W. E. Anderson, H. M. Ryan, R. J. Santoro, and R. A. Hewitt, Combustion Instability Mechanisms in Liquid Rocket Engines Using Impinging Jet Injectors, AIAA Paper 95-2357. Groning, 2016, Injector-driven combustion instabilities in a hydrogen/oxygen rocket combustor, J. Propul. Power, 32, 560, 10.2514/1.B35768 Armbruster, 2018, Experimental investigation of self-excited combustion instabilities with injection coupling in cryogenic rocket combustor, Acta Astronaut., 151, 655, 10.1016/j.actaastro.2018.06.057 Richecoeur, 2008, Experimental investigation of high-frequency combustion instabilities in liquid rocket engine, Acta Astronaut., 62, 18, 10.1016/j.actaastro.2006.12.034 Urbano, 2016, Exploration of combustion instability triggering using large eddy simulation of a multiple injector liquid rocket engine, Combust. Flame, 169, 129, 10.1016/j.combustflame.2016.03.020 Bai, 2020, Effects of self-pulsation on combustion instability in a liquid rocket engine, Exp. Therm. Fluid Sci., 114, 110038, 10.1016/j.expthermflusci.2019.110038 Xue, 2020, Experimental investigation of self-excited combustion instabilities in a small earth storable bipropellant rocket combustor, Aero. Sci. Technol., 105, 106008, 10.1016/j.ast.2020.106008 Takeno, 1968, 420 Anand, 2018, Rotating detonation wave mechanisms through ethylene-air mixtures in hollow combustors, and implications to high frequency combustion, Exp. Therm. Fluid Sci., 92, 314, 10.1016/j.expthermflusci.2017.12.004 Anand, 2019, Rotating detonation combustors and their similarities to rocket instabilities, Prog. Energy Combust. Sci., 73, 182, 10.1016/j.pecs.2019.04.001 Lawhead, 1961, Photographic studies of combustion processes in liquid propellant rockets, vol. 8, 1140 Rupe, 1965 Kanda, 2019, Off-design combustion in liquid-propellant rocket engine with high-frequency instability, Trans. JSASS, 62, 331 T. Kanda, S. Kikuchi, and H. Kinoh, Experimental Validation of Off-Design Combustion for Liquid-Propellant Rocket Engine High-Frequency Instability, to Be Published from Trans. JSASS.