1 |
Bae, S.H., Jung, H. and Kim, J.S., "A Preliminary Configuration Design of Methane/Oxygen Bipropellant Small-rocketengine through Theoretical Performance Analysis," Journal of the Korean Society of Propulsion Engineers, Vol. 19, No. 3, pp. 47-53, 2015.
DOI
|
2 |
Bostwick, C., Gibbs, T. and Anusha, P., "LOX/Methane Engine Utilizing Liquid/Liquid Co-axial Swirl Injector," 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, F.L., U.S.A., AIAA 2011-838, Jan. 2011.
|
3 |
Ramezani, A.R. and Ghafourian, A., "Spray Angle Variation of Liquid-Liquid Swirl Coaxial Injector," 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Tucson, A.Z., U.S.A., AIAA 2005-3747, July 2005.
|
4 |
Yang, L.J. and Ge, M.H., "Spray Characteristics of a Recessed Gas-Liquid Coaxial Swirl Injecrot," Journal of Propulsion and Power, Vol. 24, No. 6, pp. 1332-1339, 2008.
DOI
|
5 |
Jeon, J.H., Hong, M.G., Han, Y.M. and Lee, S.Y., "Experimental Study on Spray Characteristics of Gas-Centered Swirl Coaxial Injectors," Journal of Fluids Engineering, Vol. 133, No. 12, pp. 121303-1-7, 2011.
DOI
|
6 |
Kim, S.H. and Yoon, J.S., "Experimental Study on the Internal Flow Characteristics for Recess Length in a Swirl Coaxial Injector," 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Nashville, T.N., U.S.A., AIAA 2010-6812, July 2010.
|
7 |
Tamaki, N., Shimizu, M., Nishida, K. and Hiroyasu, H., "Effects of Cavitation and Internal Flow on Atomization of a Liquid Jet," Atomization and Sprays, Vol. 8, No. 2, pp. 179-197, 1998.
DOI
|
8 |
Hiroyasu, H., "Spray Break-up Mechanism from the Hole-type Nozzle and Its Applications," Atomization and Sprays, Vol. 10, No. 3-5, pp. 511-527, 2000.
DOI
|
9 |
Kent, J.C. and Brown, G.M., "Nozzle Exit Flow Characteristics for Square-edged and Rounded Inlet Geometries," Combustion Science and Technology, Vol. 30, No. 1-6, pp. 121-132, 1983.
DOI
|
10 |
Ganippa, L.C., Bark, G., Andersson, S. and Chomiak, J., "Cavitation: A Contributory Factor in the Transition from Symmetric to Asymmetric Jets in Cross-flow Nozzles," Experiments in Fluids, Vol. 36, No. 4, pp. 627-634, 2004.
DOI
|
11 |
Hun, J., Kim, J.H. and Kim, J.S., "Spray Characteristics of Nonimpinging-type Injector According to the Injection Pressure Variation and Angular Direction of Orifices ," Journal of the Korean Society of Propulsion Engineers, Vol. 16, No. 3, pp. 1-8, 2016.
DOI
|
12 |
Lefebvre, A.H., Atomization and Sprays, Taylor & Francis, New York, N.Y., U.S.A., 1989.
|
13 |
Kenny, R.J., Moser, M.D., Hulka, J. and Jones, G., "Cold Flow Testing for Liquid Propellant Rocket Injector Scaling and Throttling," AIAA-2006-4705, 2006.
|
14 |
Stiesch, G., Modeling Engine Spray and Combustion Processes, Springer, Berlin, pp.119-192, 2003.
|