[1] |
刘国球.液体火箭发动机原理[M].北京: 宇航出版社, 1993: 251-252.Liu G Q.The Princple of liquid rocket engine[M].Beijing: Astronautic Publishing House, 1993: 251-252(in Chinese).
|
[2] |
Zinn B T. Pulsating combustion, advanced combustion methods[M].London: Academic Press, 1986: 113-181.
|
[3] |
Culick F E C.A note on Rayleigh's criterion[J].Combustion Science and Technology, 1987, 56(4-6): 159-166.
|
[4] |
Habiballah M, Lourme D, Pit F.A comprehensive model for combustion stability studies applied to the Ariane Viking engine, AIAA-1988-0086[R].Reston: AIAA, 1988: 1-7.
|
[5] |
尕永婧, 张会强, 王希麟.隔板对燃烧室压力高频自激振荡的抑制作用[J].清华大学学报, 2012, 52(7): 1007-1012. Ga Y J, Zhang H Q, Wang X L.Effects of baffles on self-triggered high frequency pressure oscillations in a thrust chamber[J].Journal of Tsinghua University, 2012, 52(7): 1007-1012(in Chinese).
|
[6] |
Matthew E H, William E A, Charles L M.Analysis of self-excited combustion instabilities using two-and three-dimensional simulations[J].Journal of Propulsion and Power, 2013, 29(2): 396-409.
|
[7] |
Pieringer J, Sattelmayer T, Fassl F.Simulation of combustion instabilities in liquid rocket engines with acoustic perturbation equations [J].Journal of Propulsion and Power, 2009, 25(5): 1020-1031.
|
[8] |
Oberger C L, Hines W S, Falk A Y.High-temperature earth-storable propellant acoustic cavity technology, NASA N75-19460[R].California: Rocketdyne Division, 1974: 1-82.
|
[9] |
Kim J S. Effects of turbulence on linear acoustic instability: Spatial inhomogeneity[C]//Progress in Aeronautics and Astronautics.Reston: AIAA, 1995, 169: 431-454.
|
[10] |
Ewert R, Schröder W.Acoustic perturbation equations based on flow decomposition via source filtering[J].Journal of Computational Physics, 2003, 188(2): 365-398.
|
[11] |
Laroche E, Habiballah M, Kuentzmann P.Numerical analysis of liquid rocket combustion instability: Preliminary 3D acoustic calculations[C]//35th Intersociety Energy Conversion Engineering Conference and Exhibit. Reston: AIAA, 2000: 1-9.
|
[12] |
Tam C K W, Webb J C.Dispersion-relation-preserving finite difference schemes for computational acoustics[J].Journal of Computational Physics, 1993, 107(2): 262-281.
|
[13] |
Gaitonde D V, Visbal M R.Padé-type higher-order boundary filters for the Navier-Stoke equations[J].AIAA Journal, 2000, 38(11): 2103-2112.
|
[14] |
Tam C K W, Dong Z.Wall boundary conditions for high-order finite-difference schemes in computational aeroacoustics[J].Theoretical and Computional Fluid Dynamics, 1994, 6(5-6): 303-322.
|
[15] |
Laudien E, Pongratz R, Pierro R, et al.Experimental procedures aiding the design of acoustic cavities[C]//Progress in Aeronautics and Astronautics.Reston: AIAA, 1995, 169: 377-402.
|
[16] |
Harrje D T, Reardon F H.Liquid rocket combustion instabilities, NASA SP-194[R].Reston: AIAA, 1972.
|
[17] |
Milano D, Kirkpatrick A T, Quinlan J M, et al.Computation of acoustic oscillations and combustion stability in a rocket engine with combined hub/blade baffles, AIAA-2009-4866[R].Reston: AIAA, 2009.
|