1 |
Lehoucq, R. and Sorensen, D., "ARPACK.User's Guide: Solution of Large Scale EigenvalueProblems with Implicitly Restarted Arnoldi Methods",www.caam.rice.edu/software/ARPACK, 1997.
|
2 |
Crocco, L. and Cheng, S., "Theory ofCombustion Instability in Liquid PropellantRocket Motors", Butterworths, London, 1956.
|
3 |
Portillo, J. E. and Sisco, J. C., "Generalized Combustion Instability Model", AIAA-2006-4889, 2006.
|
4 |
Lieuwen, T., "Modeling Premixed Combustion-Acoustic Wave Interactions: A Review", Journal of Propulsion and Power, Vol. 19, No. 5, 2003, pp. 765-781.
DOI
ScienceOn
|
5 |
Smith, R., Ellis, M., Xia, G., Sankaran, V.,Anderson, W., and Merkle, C., L., "ComputationalInvestigation of Acoustics and Instabilities in aLongitudinal-Mode Rocket Combustor", AIAAJournal, Vol. 46, No. 11, 2008, pp. 2659-2673.
DOI
ScienceOn
|
6 |
김성구, 박태선, "시간지연 모델을 이용한 액체로켓엔진의 축방향 비선형 연소불안정 해석", KARI-REG-TM-2004-039, 한국항공우주연구원.
|
7 |
Day, D. and Heroux, M. A., "Solvingcomplex valued linear systems via equivalentreal formulations", SIAM J. Sci. Comput., Vol.23, No. 2, 2001, pp. 480-498.
DOI
ScienceOn
|
8 |
Munankarmy, A. and Heroux, M. A.,"Comparison of two equivalent real formulationsfor complex-valued linear systems", AmericanJournal of Undergraduate Research, Vol. 1, No. 3,2002, pp. 17-25.
|
9 |
Saad, Y., "SPARSKIT: a Basic Tool Kit forSparse Matrix Computations, Version 2", 1994.
|
10 |
고영성, 이광진, 김홍집, "액체로켓엔진 연소실에서의 상온 음향 시험", 대한기계학회논문집B, 제28권 제1호, 2004, pp. 16-23.
과학기술학회마을
DOI
ScienceOn
|
11 |
Pierringer, J., Sattelmayer, T., and Fassl,F., "Simulation of Combustion Instabilities inLiquid Rocket Engines with Acoustic PerturbationEquations", Journal of Propulsion and Power, Vol.25, No. 5, 2009, pp. 1020-1031.
DOI
ScienceOn
|
12 |
Nicoud, F., Benoit, L., Sensiau, C., andPoinsot, T., "Acoustic Modes in Combustors withComplex Impedances and MultidimensionalActive Flames", AIAA Journal, Vol. 45, No. 2,2007, pp. 426-441.
DOI
ScienceOn
|
13 |
Sensiau, C., Nicoud, F., van Gijzen, M.,and Leeuwen, J. W., “A Comparison of Solversfor Quadratic Eigenvalue Problems fromCombustion", International Journal for NumericalMethods in Fluids, Vol. 56, 2008, pp. 1481-1487.
DOI
ScienceOn
|
14 |
Giauque, A., Selle, L., Poinsot, T., Buechner, H., Kaufmann, P., and Krebs, W., "System identification of a large-scale swirled partially premixed combustor using LES and measurements", Journal of Turbulence, Vol. 6, No. 21, 2005, pp. 1-20.
DOI
ScienceOn
|
15 |
Huang, Y. and Yang, V., "Dynamics andstability of lean-premixed swirl-stabilizedcombustion", Progress in Energy and CombustionScience, Vol. 35, No. 4, 2009, pp. 293-364.
DOI
ScienceOn
|
16 |
김성구, 김홍집, 손채훈, "로켓엔진 연소기 설계의 음향안정성 평가를 위한 해석코드 개발", 한국항공우주학회지, 제32권 제6호, 2004, pp. 110-116.
|
17 |
김홍집, 김성구, "로켓연소실에서 음향공의 음향학적 감쇠에 대한 정량적 고찰", 대한기계학회논문집B, 제30권 제1호, 2006, pp. 32-40.
과학기술학회마을
DOI
ScienceOn
|
18 |
김홍집, 김성구, 한영민, 최환석, "비행용 가스발생기 모사배관 도출 및 연소불안정 제어를 위한 음향해석", 한국추진공학회지, 제9권 제3호, 2005, pp. 1-9.
과학기술학회마을
|
19 |
Sohn, C. H., Park, I-S., Kim, S.-K., andKim, H. J., "Acoustic Tuning of Gas-LiquidScheme Injectors for Acoustic Damping in aCombustion Chamber of a Liquid RocketEngine", Journal of Sound and Vibration, Vol.304, 2007, pp. 793-810.
DOI
ScienceOn
|
20 |
Yang, V. and Anderson, W. E. (eds),"Liquid Rocket Engine Combustion Instability",Progress in Astronautics and Aeronautics, Vol 169,AIAA, 1995.
|
21 |
Lieuwen, T. C. and Yang, V. (eds),"Combustion Instabilities in Gas Turbine Engines",Progress in Astronautics and Aeronautics, Vol 210,AIAA, 2005.
|
22 |
Stow, S. and Dowling, A., "ThermoacousticOscillations in an Annular Combustor",ASME Turbo Expo, 2001-GT-0037.
|
23 |
Pankiewitz, C. and Sattelmayer, T., "TimeDomain Simulation of Combustion Instabilitiesin Annular Combustors", Journal of Engineeringfor Gas Turbines and Power, Vol. 125, No. 3,2003, pp. 677-685.
DOI
ScienceOn
|
24 |
Cha, D. J., Kim, J. H., and Joo, Y. J.,"Analysis of the Combustion Instability of aModel Gas Turbine Combustor by the TransferMatrix Method", Journal of Mechanical Scienceand Technology, Vol. 23, 2009, pp. 1602-1612.
DOI
ScienceOn
|