1 |
J. Cui, H. Lai, J. Li and Y. Ma, "Visualization of internal flow and the effect of orifice geometry on the characteristics of spray and flow field in pressure-swirl atomizers", Applied Thermal Engineering, Vol. 127, 2017, pp. 812-822.
DOI
|
2 |
S. Yao, J. Zhang and T. Fang, "Effect of viscosities on structure and instability of sprays from a swirl atomizer", Experimental Thermal and Fluid Science, Vol. 39, 2012, pp. 158-166.
DOI
|
3 |
S. Kim, D. Kim, T. Khil and Y. Yoon, "Effect of geometry on the liquid film thickness and formation of air core in a swirl injector", 43rd AIAA/ASME/SAE/ASEE, Joint Propulsion Conference & Exhibit, 2007.
|
4 |
S. Kim, T. Khil, D. Kim and Y. Yoon, "Effect of geometric parameters on the liquid film thickness and air core formation in a swirl injector", Measurement Science and Technology, Vol. 20, 2009, 015403.
DOI
|
5 |
S. Oh, G. Park, S. Kim, H. Lee, Y. Yoon and J. Y. Choi, "A study on dynamic characteristics of gas-centered swirl coaxial injector varying tangential inlet diameter with liquid pulsation", Journal of ILASS-Korea, Vol. 22, No. 2, 2017, pp. 62-68.
DOI
|
6 |
B. Sumer, N. Erkan, O. Uzol and I. H. Tuncer, "Experimental and numerical investigation of a pressure swirl atomizer", 12th Triennial International Conference on Liquid Atomization and Conference on Liquid Atomization and Spray System, 2012.
|
7 |
J. Zhao and L. Yang, "Simulation and experimental study on the atomization character of the pressure-swirl nozzle", Open Journal of Fluid Dynamics, Vol. 2, 2012, pp. 271-277.
DOI
|
8 |
J. Y. Kim, Y. Yoon and J. Y. Choi, "Numerical analysis of internal flow of closed-type swirl injector using VOF method", Korean Society of Propulsion Engineering Fall Conference Paper, 2016, pp. 419-421.
|
9 |
W. Yoon, "A study on the spray characteristics of biswirl injectors", Master Thesis, Chungbuk National University, 2017.
|
10 |
W. Yoon, B. Lee and K. Ahn, "A study on the spray characteristics of swirl injectors using ANSYS Fluent", Journal of ILASS-Korea, Vol. 22, No. 4, 2017, pp. 159-168.
DOI
|
11 |
ANSYS Fluent Theory Guide, v17.2, Canonsburg, PA, 2016.
|
12 |
ANSYS Fluent User's Guide, v17.2, Canonsburg, PA, 2016.
|
13 |
G. P. Sutton, Rocket Propulsion Elements, 6th ed., John Wiley & Sons Inc., New York, 1992.
|
14 |
T. Marchione, C. Allouis, A. Amoresano and F. Beretta, "Experimental investigation of a pressure swirl atomizer spray", Journal of Propulsion and Power, Vol. 23, No. 5, 2007, pp. 1096-1101.
DOI
|
15 |
D. K. Huzel and D. H. Huang, Modern engineering for design of liquid-propellant rocket engines, 2nd ed., AIAA, Washington D.C., 1992.
|
16 |
A. H. Lefebvre, Atomization and Sprays, Hemisphere Publishing Corp., New York, 1989.
|
17 |
V. G. Bazarov, Liquid Injector Dynamics, Moscow, Mashinostrenie, 1979.
|
18 |
Y. Chung, H. Kim, S. Jeong and Y. Yoon, "Dynamic characteristics of open-type swirl injector with varying geometry", Journal of Propulsion and Power, Vol. 32, No. 3, 2016, pp. 583-591.
DOI
|
19 |
Q. F. Fu, L. J. Yang and X. D. Wang, "Theoretical and experimental study of the Dynamics of a liquid swirl injector", Journal of Propulsion and Power, Vol. 26, No. 1, 2010, pp. 94-101.
DOI
|
20 |
Q. F. Fu, L. J. Yang and Y. Y. Qu, "Measurement of annular liquid film thickness in an open-end swirl injector", Aerospace Science and Technology, Vol. 15, No. 2, 2011, pp. 117-124.
DOI
|
21 |
C. Chen, Y. Yang, S. H. Yang and H. L. Gao, "The spray characteristics of an open-end swirl injector at ambient pressure", Aerospace Science and Technology, Vol. 67, 2017, pp. 78-87.
DOI
|
22 |
M. Rashad, H. Yong and Z. Zekun, "Effect of geometric parameters on spray characteristics of pressure swirl atomizers", International Journal of Hydrogen Energy, Vol. 41, 2016, pp. 15790-15799.
DOI
|
23 |
T. Inamura, H. Tamura and H. Sakamoto, "Characteristics of liquid film and spray injected from swirl coaxial injector", Journal of Propulsion and Power, Vol. 19, No. 4, 2003, pp. 632-639.
DOI
|
24 |
Q. F. Fu and L. J. Yang, "Visualization studies of the spray from swirl injectors under elevated ambient pressure", Aerospace Science and Technology, Vol. 47, 2015, pp. 154-163.
DOI
|