1 |
Rizk, N. K. and Lefebvre, A. H., "Spray characteristics of simplex swirl atomizer", Dynamics of Flames and Reactive Systems(J. R. Bowen, N. Manson, A. K. Oppenheim and R. I. Soloukhin, Eds), Progress in Astronautics and Aeronautics, 95, 1984
|
2 |
V. Barzarov, "lecture on liquid propellant rocket engine injectors", Seoul National University, Jan. 28-Feb. 8, 2002
|
3 |
G. P. Sutton, "Rocket propulsion elements", Seventh Edition, 2001, pp.197-265
|
4 |
L. Schoenman, "Fuel/oxidizer-rich high-pressure preburners," NASA CR 165404, Octorber, l981
|
5 |
양준호, 최성만, "로켓 산화제 과잉 예연소기 분사기의 성능특성 연구", 한국추진공학회지, 제11권 제1호, 2007, pp.57-63
과학기술학회마을
|
6 |
X. F Wang and A. H Lefebvre "Influence of ambient air pressure on pressure-swirl atomization" Atomization and Spray Technology 3, 1987, pp.209-226
|
7 |
Abou-Ellail, M. M. M., Elkotb, M. M. and Rafat, N. M., "Effect of fuel pressure, air pressure and air temperature on droplet size distribution in hollow-cone kerosine sprays", 1st International Conference on Liquid Atomization and Spray Systems, ICLASS-78, Tokyo, 1978, pp.85-92
|
8 |
Dodge, L. G., "Effect of elevated temperature and pressure on sprays from simplex swirl atomizers", ASME Paper 85-GT-58, presented at 30th Internation Gas Turbine Conference, Houston, Texas, March, 1985, pp.18-21
|
9 |
우주발사체사업단, "우주발사체 기술강좌", 한국항공우주연구원, Oct. 29-Nov. 2, 2007
|
10 |
V. Barzarov, "Development of russian rocketry-historical and technical aspects", 6th NRL Workshop, Issues on Rocket Engine, 2005
|
11 |
Neya, K. and Sato, S., "Effect of ambient air pressure on the spray characteristics of swirl atomizers", Ship Res. Inst. Tokyo, paper 27, 1968
|