1 |
Huang Yuhui, 'Acoustic Model for the Self-oscillation of Coaxial Swirl Injector', 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Seattle, WA, 1997
|
2 |
박이선, 손채훈, '액체 로켓엔진 분사기의 음향감쇠 효과에 관한 수치적 연구', 한국항공우주학회지, 제 33권, 제 5호, 2005
DOI
|
3 |
Laudien, E., Pongratz, R, and Preclik, D., in Liquid Rocket Engine Combustion Instability (Yang, V. and Anderson, W. E.m eds), Progress in Astronautics and Aeronautics, Vol. 169, AIAA, Washington DC, 1995, pp. 377-399
|
4 |
Culick, F.E.C. and Yang, V., 'Overview of Combustion Instabilities in Liquid-Propellant Rocket Engines', Progress in Astronautics and Aeronautics, Vol. 169, 1995
|
5 |
Harrje, D. T. and Reardon, F. H., (eds) Liquid Propellant Rocket Combustion Instability, NASA SP-194,1972
|
6 |
Zucrow, M. J. and Hoffman, J. D., Gas Dynamics vol. II, Multicimensional Flow, John Wiley and Sons, Inc., 1977
|
7 |
Kinsler, L. E., Frey, A. R, Coppens, A. B. and Sanders, J. V., Fundamentals of Acoustics, 4th ed. John Wiley & Sons, Inc., 2000
|
8 |
V.G. Bazarov, Liquid Propellant Rocket Engine Injectors, Invited Lecture of V. Bazarov, Rocket Propulsion Lab., Seoul National University, 2002
|
9 |
V. G. Bazarov, Liquid Injector Dynamics, Moscow, Mashinostroenie, 1979
|
10 |
Hwang, Seong-Ha, Backhole as a New Geometric Parameter and Acoustic Damper for the Swirl Injector, Mater thesis, Soul National University, 2004
|