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2026 Vol.30, Issue 2 Preview Page

RESEARCH PAPERS

30 April 2026. pp. 38-49
Abstract
References
1

Sutton, G. P., and Biblarz O. Rocket Propulsion Elements, John Wiley & Sons Inc., New York, NY, USA, 2001.

2

Wu, K., Kim, T. H., and Kim, H .D., “Theoretical and Numerical Analyses of Aerodynamic Characteristics on Shock Vector Control,” Journal of Aerospace Engineering, Vol. 33, No. 5, 2020, p. 04020050 (1-27).

10.1061/(ASCE)AS.1943-5525.0001169
3

Chouicha, R., Sellam, M., and Bergheul, S., “Effect of Reacting Gas on the Fluidic Thrust Vectoring of an Axisymmetric Nozzle,” Propulsion and Power Research, 2020.

10.1016/j.jppr.2020.04.002
4

Hakim, K., Toufik, H., and Said, B., “Numerical Simulation of Fluidic Thrust Vectoring in the Conical Nozzle,” Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, Vol. 73, No. 2, 2020, pp. 88-105.

10.37934/arfmts.73.2.88105
5

Wu, K., Kim, T., and Kim, H., “Sensitivity Analysis of Counterflow Thrust Vector Control with a Three-dimensional Rectangular Nozzle,” Journal of Aerospace Engineering, Vol. 34, No. 1, 2021, p. 04020107 (1-16).

10.1061/(ASCE)AS.1943-5525.0001228
6

Wu, K., and Kim, H. D., “Fluidic Thrust Vector Control Using Shock Wave Concept,” Journal of the Korean Society of Propulsion Engineers, Vol. 23, No. 4, 2019, pp. 10-20.

10.6108/KSPE.2019.23.4.010
7

Hojaji, M., Razavi Dehkordi, M. H., and Hosseini, S. A., “Experimental Study of the Effects of Secondary Flow Injection on the Exhaust Flow of Converging - Diverging Nozzles at Different Oblique Angles,” Journal of Aeronautic Engineering, Vol. 24, No. 1, 2022, pp. 45-56.

8

Lin W., Shi Q., Liu S., Lin Z., Tong Y., and Su L., “Study of Thrust Vector Control for the Rotating Detonation Model Engine,” International Journal of Hydrogen Energy, Vol. 47, No. 2, 2022, pp. 1292-1305.

10.1016/j.ijhydene.2021.10.050
9

Rose, D. B. B., and Sridhar, B., “A Rectangular Strut on the Expansion Ramp of a Scramjet thruster for Thrust Vector Control,” Acta Astronautica, Vol. 194, 2022, pp. 9-21.

10.1016/j.actaastro.2022.01.041
10

Xia, H., Wang, P., Dong, H., Jin, Z., An, X., and Fang, L., “Hydrodynamic Characteristics of a New Thrust Vectoring Ducted Propeller with Slotted Nozzle,” Ocean Engineering, Vol. 266, 2022.

10.1016/j.oceaneng.2022.112805
11

Wu, K., “Study on Aerodynamic Features of Rod Thrust Vector Control for Physical Applications,” Proceedings of the Institution of Mechanical Engineers, Part G/Journal of Aerospace Engineering, Vol. 237, No. 1, 2023, pp. 156-176.

10.1177/09544100221095363
12

Kostić, O., Stefanović, Z., and Kostić, I., “Comparative CFD Analyses of A 2D Supersonic Nozzle Flow with Jet Tab and Jet Vane,” Technical Gazette, Vol. 24, No. 5, 2017, pp. 1335-1344.

10.17559/TV-20160208145336
13

Deere, K. A., “Summary of Fluidic Thrust Vectoring Research Conducted at NASA Langley Research Center,” 21st AIAA Applied Aerodynamics Conference, Orlando, FL, USA, AIAA 2003-3800, Jun 2003.

10.2514/6.2003-3800
14

Lee, Y., Park, S., and Kim, Y., “Thrust Vectoring of Sonic Jet by Using Coanda Flap and Solenoid Valve,” AIAA Journal, Vol. 54, No. 9, 2016, pp. 2909-2915.

10.2514/1.J054993
15

Lee, M., Song, M., Kim, D., and Lee, Y., “Bidirectional Thrust Vectoring Control of a Rectangular Sonic Jet,” AIAA Journal, Vol. 56, No. 6, 2018, pp. 2494-2498.

10.2514/1.J056598
16

Lee, M., and Lee, Y., “Thrust Vectoring Control of Supersonic Jet Using Proportional Control Valves,” Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 47, No. 1, 2019, pp. 1-8.

10.5139/JKSAS.2019.47.1.1
17

Burnazzi, M., and Radespiel, R., “Design and Analysis of a Droop Nose for Coanda Flap Applications,” Journal of Aircraft, Vol. 51, No. 5, 2014, pp. 1567-1579.

10.2514/1.C032434
18

Jojić, B., Stefanović, Z., Blagojević, Đ., Vučković, S., and Rajčić, Z., “Research in Modern Rocket Propulsion TVC,” University of Belgrade, Faculty of Mechanical Engineering and VTI Žarkovo, Belgrade, Serbia, 1984.

19

Jojić, B., Milinović, M., Stefanović, Z., and Blagojević, Đ., “Pressure Distribution in Rocket Nozzle with Mechanical System for TVC,” AIAA Paper 87-1824, USA, 1987.

20

Stefanović, Z., “Research of Fluid Flow and Pressure Distribution in Supersonic Nozzle in Connection with the Vector Thrust Control,” Doctoral Thesis, University of Belgrade, Belgrade, Serbia, 1986.

21

Stefanović, Z., Miloš, M., Todić, I., and Pavlović, M., “Investigation of the Pressure Distribution in a 2D Rocket Nozzle with a Mechanical System for Thrust Vector Control (TVC),” Strojarstvo, Vol. 53, No. 4, 2011, pp. 287-292.

22

ANSYS FLUENT 22, Theory Guide, ANSYS, Inc., Canonsburg, PA 15317 USA, 2022.

23

Menter, F. R., “Two-Equation Eddy Viscosity Turbulence Models for Engineering Applications”, AIAA Journal, Vol. 32, No. 8, 1994, pp. 1598-1605.

10.2514/3.12149
24

Kim, S. D., and Song, D. J., “Modified Shear-Stress Transport Turbulence Model for Supersonic Flows,” Journal of Aircraft, Vol. 42, No. 5, 2005, pp. 1118-1125.

10.2514/1.10223
25

Menter, F. R., “Review of the SST Turbulence Model Experience from an Industrial Perspective,” International Journal of Computational Fluid Dynamics, Vol. 23, No. 4, 2009, pp. 305-316.

10.1080/10618560902773387
Information
  • Publisher :The Korean Society of Propulsion Engineers
  • Publisher(Ko) :한국추진공학회
  • Journal Title :Journal of the Korean Society of Propulsion Engineers
  • Journal Title(Ko) :한국추진공학회지
  • Volume : 30
  • No :2
  • Pages :38-49
  • Received Date : 2025-12-07
  • Revised Date : 2026-03-18
  • Accepted Date : 2026-03-18