참고문헌 (17)

1. Harrje, D. J. and Reardon, F. H.(eds.), Liquid Propellant Rocket Instability, NASA SP-194, 1972. 

2. Huzel, D. K., and Huang, D. H., Modern Engineering for Design of Liquid-Propellant Rocket Engines, volume 147, Progress in Astronautics and Aeronautics, AIAA, Washington D. C., 1992. 

3. Culick, F. E. C., and Yang, V., "Overview of Combustion Instabilities in Liquid-Propellant Rocket Engines," in Liquid Rocket Engine Combustion Instability, volume 169, Progress in Astronautics and Aeronautics, AIAA, Washington D. C., 1995, pp. 3-38. 

4. 윤명원, 윤재건, "액체 로켓 추진기관의 연소불안정 현상", 한국항공우주학회지, 제25권, 제5호, 1997, pp. 183-189. 

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5. 윤웅섭, 허환일, "액체로켓엔진 고주파 연소불안정의 예측", 한국추진공학회지, 제7권, 제3호, 2003, pp. 61-68. 

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6. Agarkov, A. F., Denisov, K. P., Dranovsky, M. L., Zavorohin, I. A., Ivanov, V. N., Pikalov, V. P., and Shibanov, A. A., "Injector Flame Stabilization Effects on Combustion Instability," in Liquid Rocket Engine Combustion Instability, volume 169, Progress in Astronautics and Aeronautics, AIAA, Washington D. C., 1995, pp. 281-305. 

7. Crocco, L., "Theoretical Studies on Liquid Propellant Rocket Instability," 10th Symposium on Combustion, The Combustion Institute, Pittsburgh, PA, 1965, pp. 1101-1128. 

8. Sirignano, W. A., and Law, C. K., "Transient Heating and Liquid-Phase Mass Diffusion in Fuel Droplet Vaporization," Evaporation and Combustion of Fuels, Advances in Chemistry Series, volume 166, American Chemical Society, New York, 1978, pp. 1-26. 

9. Habiballah, I. O., "Modified Two-Level State Estimation Approach", IEE Proceedings, Part C, volume 143, No. 2, 1996, pp. 193-199. 

10. Dubois, I., and Habiballah, M., "Numerical Simulation of High Frequency Instability in an Oxygen/Hydrogen Rocket Engines," AIAA Paper 91-1860, 1991. 

11. Jeng, S., Keefer, D., Welle, R., Peters, C., "Laser-Sustained Plasma in Forced Convective Argon Flow, Part II: Comparison of Numerical Model with Experiment," AIAA Journal, volume 25, No. 9, 1987, pp. 1224-1229. 

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12. Yoon, W. S. and Chung, T. J., "Liquid Propellant Combustion Waves," AIAA paper 91-2088, 1991. 

13. Sohn, C. H., Chung, S. H., Kim, J. S., and Williams, F. A., "Acoustic Response of Droplet Flames to Pressure Oscillations," AIAA Journal, volume 34, No. 9, 1996, pp. 1847-1854. 

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14. 김성구, 김홍집, 손채훈, "로켓엔진연소기 설계의 음향안정성 평가를 위한 해석코드 개발", 한국항공우주학회지, 제31권, 제6호, 2003, pp. 110-116. 

15. Sohn, C. H., Kim, S. K., and Kim, Y. M., "A Numerical Study on Effects of Various Baffle Designs on Acoustic Characteristics in Combustion Chamber of Liquid Rocket Engine," KSME International Journal, Vol. 18, No. 1, 2004, pp. 145-152. 

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16. Combs, L. P., Oberg, C. L., Coultas, T. A., and Evers, W. H., Jr., Liquid Rocket Engine Combustion Stabilization Devices, NASA SP-8113, 1974. 

17. 손채훈, 김성구, 문윤완, 김영목, 위성 발사체 로켓엔진의 연소 불안정 억제/방지기술, 한국항공우주연구원, 2003. 

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