| [1] Im J H, Kim D, Yoon Y, et al. Self-pulsation characteristics of a swirl coaxial injector with various injection and geometric conditions, AIAA-2005-3749[R]. Reston: AIAA, 2005.[2] Yoshio N, Hiroshi S, Hiroshi T, et al. An experimental study of super-pulsating flow on a shear coaxial injector with a recessed inner post, AIAA-2007-5560[R]. Reston: AIAA, 2007.[3] Yoshio N, Hiroshi T, Takuo O, et al. Effect of liquid disintegration on flow instability in a recessed region of a shear coaxial injector, AIAA-2009-5389[R]. Reston: AIAA, 2009.[4] Kim B D, Heister S D. Effect of chamber pressure variation on high-frequency hydrodynamic instability of shear coaxial injector, AIAA-2004-3522[R]. Reston: AIAA, 2004.[5] Tsohas J, Heister S D. Numerical simulations of liquid rocket coaxial injector hydrodynamics[J]. Journal of Propulsion and Power, 2011, 27(4): 793-810.[6] Kim B D, Heister S D, Collicott S H. Three-dimensional flow simulations in the recessed region of a coaxial injector[J]. Journal of Propulsion and Power, 2005, 21(4): 728-742.[7] Kim B D, Heister S D. Two-phase modeling and hydrodynamic instability in coaxial injectors[J]. Journal of Propulsion and Power, 2004, 20(3): 468-479.[8] Yang L J, Fu Q F. Stability of confined gas-liquid shear flows in recessed shear coaxial injectors[J]. Journal of Propulsion and Power, 2012, 28(6): 1413-1424.[9] Yoon J, Chung J M, Yoon Y. Study on self-pulsation characteristics of gas/liquid shear coaxial injector with annular liquid sheets, AIAA-2012-3859[R]. Reston: AIAA, 2012.[10] Bazarov V. Self-pulsations in coaxial injectors with central swirl liquid stage, AIAA-1995-2358[R]. Reston: AIAA, 1995.[11] Bazarov V, Yang V. Liquid-propellant rocket engine injector dynamics[J]. Journal of Propulsion and Power, 1998, 14(5): 797-806.[12] Bazarov V. Influence of propellant injector stationary and dynamic parameters on high frequency combustion stability, AIAA-1996-3119[R]. Reston: AIAA, 1996.[13] Bazarov V. Non-linear interactions in liquid-propellant rocket engine injectors, AIAA-1998-4039[R]. Reston: AIAA, 1998.[14] Yang L J, Ge M H, Zhang M Z, et al. Spray characteristics of recessed gas-liquid coaxial swirl injector[J]. Journal of Propulsion and Power, 2008, 24(6): 1332-1339.[15] Sasaki M, Sakamoto H, Takahashi M, et al. Comparative study of recessed and non-recessed swirl coaxial injectors, AIAA-1997-2907[R]. Reston: AIAA, 1997.[16] Huang Y, Zhou J, Hu X, et al. Acoustic model for the self-oscillation of coaxial swirl injector, AIAA-1997-3328[R]. Reston: AIAA, 1997.[17] Chad J E, David M L, Robert A F J. Detailing the stability boundary of self-pulsations for a swirl-coaxial injector element, AIAA-2013-4064[R]. Reston: AIAA, 2013.[18] Chad J E, David M L, Robert A F J. Propellant throttling effects on self-pulsation of liquid rocket swirl-coaxial injection, AIAA-2012-4204[R]. Reston: AIAA, 2012.[19] Im J H, Kim D, Han P, et al. Self-pulsation characteristics of a gas-liquid swirl coaxial injector[J]. Atomization and Sprays, 2009, 19(1): 57-74.[20] Im J H, Yoon Y. The Effects of the ambient pressure on self-pulsation characteristics of a gas/liquid swirl coaxial injector, AIAA-2008-4850[R]. Reston: AIAA, 2008.[21] Fu Q F, Yang L J. Theoretical investigation on the dynamics of a gas-liquid coaxial swirl injector[J]. Journal of Propulsion and Power, 2011, 27(1): 144-150.[22] Im J H, Seongho C, Youngbin Y, et al. Comparative study of spray characteristics of gas-centered and liquid-centered swirl coaxial injectors[J]. Journal of Propulsion and Power, 2010, 26(6): 1196-1204.[23] Kim S, Khil T, Kim D, et al. Effect of geometric parameters on the liquid film thickness and air core formation in a swirl injector[J]. Measurement Science and Technology, 2009, 20(1): 1-11. |
CJA
