| 1 |
Y. Song, D. Hwang and K. Ahn, "Effect of orifice geometry on flow characteristics of liquid jet from single hole nozzle", Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 5, 2017, pp. 19-28./
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| 2 |
S. Joo, S. Kim, J. Yoon, J. Yoh and Y. Yoon, "A study of the flame transfer function characteristics using cold-flow transfer function in a partially premixed model gas turbine combustor", Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 5, 2017, pp. 54-60./
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| 3 |
J.M. Lim, D.S. Kim, 3D Acoustic Field Analysis in Annular Combustor System, J. Korean Soc. Propuls. Eng., 21(6) (2017) 49-56./
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| 4 |
Choi, J., and Huh, H., "Numerical Study on Transition Characteristics of Dual Bell Nozzle with Expansion Ratio Fixed," Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 3, 2017, pp.68-75./
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| 5 |
Kim, M.S., Kim, J.S., "Flame Formation of Ultrasonically-atomized Liquid-fuel Injected through a Slit-jet Nozzle," Journal of the Korean Society of Propulsion Engineers Vol. 21, No. 1, pp. 17-25, 2017./
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| 6 |
Song, J.H. and Nam, Y.K., "A Numerical Study On Thermal Characteristics of HALE UAV Solar Arrays," Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 5, pp. 29-36, 2017./
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| 7 |
Song, Y., Hwang, D. and Ahn, K., "Effect of Orifice Geometry on Flow Characteristics of Liquid Jet from Single Hole Nozzle," Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 5, pp. 19-28, 2017./
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| 8 |
Khil, T., Jung, E., Lee, K., Ryu, T. and Lee, H., "Development of Nozzleless Booster casted to Solid Propellant with Al as a Metal Fuel," Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 4, pp. 52-62, 2017./
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| 9 |
Ha, J.H., Das, R., Ladeinde, F., Kim, T.H. and Kim, H.D., "Numerical Study on Mode Transition in a Scramjet Engine," Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 6, pp. 21-31, 2017./
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| 10 |
Choi, J. and Huh, H., "Numerical Study on Transition Characteristics of Dual Bell Nozzle with Expansion Ratio Fixed," Journal of The Korean Society for Propulsion Engineers, Vol. 21, No. 3, pp. 68-75, 2017./
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