PAPERS : ACOUSTIC ANALYSIS OF LRE COMBUSTION CHAMBER WITH VARIOUS 5-BLADE BAFFLES UNDER NON-REACTING CONDITION
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Kim,Seong-Gu
Son,Chae-Hun Kim,Hong-Jip |
| 1 | Harrje, D. T. and Reardon, F. H. (eds.), 'Liquid Propellant Rocket Combustion Instability,' NASA SP-194, 1972 |
| 2 | Laudien, E., Pongratz, R., Pierro, R., and Preclik, D., in Liquid Rocket Engine Combustion Instability (Yang, V. and Anderson, W. E., eds), Progress in Astronautics and Aeronautics, Vol.169, AIAA, Washington DC, 1995, pp. 377-399 |
| 3 | 손채훈, 김성구, 문윤완, 김영목, 2003, 위성발사체 로켓엔진의 연소 불안정 억제/방지 기술, 한국항공우주연구원 |
| 4 | Yang, V., Wicker, J. M., and Yoon, M. W., in Liquid Rocket Engine Combustion Instability (Yang, V. and Anderson, W. E., eds), Progress in Astronautics and Aeronautics, Vol. 169, AIAA, Washington DC, 1995, pp. 357-376 |
| 5 | Swanson Analysis Systems, ANSYS User's Manual for revision 5.0, Volume IV, Theory, Houston, PA, 1993 |
| 6 | Sohn, C. H., Kim, S. K., and Kim, Y. M., '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 DOI |
| 7 | Wicker, J. M., Yoon, M. W., and Yang, V., 'Linear and Non-linear Pressure Oscillations in Baffled Combustion Chambers,' Journal of Sound and Vibration, Vol. 184, 1995, pp. 141-171 DOI ScienceOn |
| 8 | NASA, 'Liquid Rocket Engine Combustion Stabilization Devices,' NASA SP-8113, 1974 |
| 9 | 윤명원, 윤재건, '액체 로켓 추진기관의 연 5호, 1997, pp. 183-189 |
| 10 | 손채훈, '배플이 장착된 로켓엔진 연소기의 음향장 해석,' 대한기계학회논문집(B), 제 26권, 제 1호, 2002, pp. 966-975 |
| 11 | 고영성, 이광진, 김홍집, '액체로켓엔진 연소실에서의 상온 음향 시험,' 대한기계학회논문집(B), 제 28권, 제 1호, 2004, pp. 16-23 |
| 12 | Zucrow, M. J. and Hoffman, J. D., Gas Dynamics, Vol. II, John Wiley & Sons Inc., New York, 1977 |
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