| Citation: | TANG Guan-qiong, QIN Hao, LI Lin, LIN Yu-zhen, LI Ji-bao. Nozzle structure's influence on fuel flow oscillation in unsteady conditions[J]. Journal of Aerospace Power, 2015, 30(4): 831-837. doi: 10.13224/j.cnki.jasp.2015.04.009
|
| [1] |
Crocco L, Cheng S I.Theory of combustion instability in liquid propellant rocket motors[M].Cambridge:Cambridge University Press, 1956.
|
| [2] |
Kendirck D K, Anderson T J, Sowa W A.Acoustic sensitivities of lean-premixed rule injectors in a single nozzle rig[R].ASME Paper 98-GT-382, 1998.
|
| [3] |
Lieuwen T, Torres H, Johnson C, et al.A mechanism for combustion instabilities in premixed gas turbine combustors[J].Journal of Engineering for Gas Turbines and Power, 2000, 123(1):182-189.
|
| [4] |
Cho J H, Lieuwen T.Laminar premixed flame response to equivalence ratio oscillations[J].Combustion and Flame, 2005, 140(1):116-129.
|
| [5] |
Nguyen Q V.Measurements of equivalence ratio fluctuations in a lean premixed prevaporized (LPP) combustor and its correlation to combustion instability[R].ASME Paper GT-2002-30060, 2002.
|
| [6] |
Lieuwen T, Zinn B T.The role of equivalence ratio oscillations in driving combustion instabilities in low NOx gas turbines[J].Symposium (International) on Combustion, 1998, 27(2):1809-1816.
|
| [7] |
Lieuwen T C, Yang V.Combustion instabilities in gas turbine engines:operational experience, fundamental mechanisms and modeling[J].Progress in Astronautics and Aeronautics, 2005, 210:657-665.
|
| [8] |
Yi T, Santavicca D A.Determination of the instantaneous fuel flow rate out of a fuel nozzle[J].Journal of Engineering for Gas Turbines and Power, 2009, 132(2):021503.1-021503.7.
|
| [9] |
Yen C Y, Koeglmeier S M, Sisco J C, et al.Combustion instability of gaseous fuels in a continuously variable resonance chamber (CVRC)[R].AIAA-2008-4657, 2008.
|
| [10] |
Society of Automotive Engineers.Handbook of aviation fuel properties[M].3rd ed.Warrendale:Society of Automotive Engineers, 2004.
|
| [11] |
Karabeyoglu A, Stevens J, Cantwell B.Investigation of feed system coupled low frequency combustion instabilities in hybrid rockets[R].AIAA-2007-5366, 2007.
|
| [12] |
杨立军, 张向阳, 高芳, 等.液体喷嘴动态特性数值模拟[J].航空动力学报, 2004, 19(6):866-872. YANG Lijun, ZHANG Xiangyang, GAO Fang, et al.Numerical simulation of liquid injector dynamics[J].Journal of Aerospace Power, 2004, 19(6):866-872.(in Chinese)
|
| [13] |
李龙飞, 陈建华, 周立新, 等.补燃循环火箭发动机气液同轴式喷嘴声学特性研究[J].火箭推进, 2004, 30(6):5-10. LI Longfei, CHEN Jianhua, ZHOU Lixin, et al.Investigation on acoustic characteristics of gas-liquid coaxial injector of staged combustion rocket engine[J].Journal of Rocket Propulsion, 2004, 30(6):5-10.(in Chinese)
|
| [14] |
Huang Y, Yang V.Dynamics and stability of lean-premixed swirl-stabilized combustion[J].Progress in Energy and Combustion Science, 2009, 35(4):293-364.
|
| [15] |
Huber A, Polifke W.Impact of fuel supply impedance on combustion stability of gas turbines[R].ASME Paper GT-2008-51193, 2008.
|
| [16] |
Yi T, Santavicca D A.Flame transfer functions for liquid-fueled swirl-stabilized turbulent lean direct fuel injection combustion[J].Journal of Engineering for Gas Turbines and Power, 2009, 132(2):021506.1-021506.6.
|
| [17] |
Lichtarowicz A, Duggins R K, Markland E.Discharge coefficients for incompressible non-cavitating flow through long orifices[J].Journal of Mechanical Engineering Science, 1965, 7(2):210-219.
|
| [18] |
Lefebvre A H.Atomization and sprays[M].Boca Raton:CRC Press, 1989.
|
| [19] |
Asihmin V I, Geller Z I, Skobel'cyn Y A.Discharge of a real fluid from cylindrical orifices[J].Oil Industry, 1961, 9:135-172.
|
| [20] |
Kim H, Lai M C.Effect of pressure pulsation on performance of airblast atomizer and micro-machined fuel injectors[R].AIAA-2002-4227, 2002.
|
| [21] |
Eckstein J.On the mechanisms of combustion driven low-frequency oscillations in aero-engines[D].Munich, Germany:University of Munich, 2004.
|
DownLoad: