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Study on Fluidic Thrust Vector Control Based on Dual-Throat Concept

이중목 노즐 개념에 기반한 유체 추력벡터제어에 관한 연구

  • Wu, Kexin (Department of Mechanical Engineering, Andong National University) ;
  • Kim, Heuy Dong (Department of Mechanical Engineering, Andong National University)
  • Received : 2018.06.20
  • Accepted : 2019.01.06
  • Published : 2019.02.01

Abstract

Numerical simulations were carried out in a supersonic nozzle to investigate the possibility of using dual-throat nozzle concept in fluidic thrust vector control. Validation of the methodology showed an excellent agreement between the computational fluid dynamics results and the experimental data available, which were based on the well-assessed SST $k-{\omega}$ turbulence mode. The deflection angle, system resultant thrust ratio, and thrust efficiency were investigated in a wide range of nozzle pressure ratios and injection pressure ratios. The performance variations of the dual-throat nozzle thrust vector control system were clearly illustrated with this two-dimensional computational domain. Some constructive conclusions were obtained that may be used as a reference for further studies in the fluidic thrust vector control field.

유체 추력벡터 제어에서 이중목 노즐 개념의 이용 가능성을 조사하기 위하여, 초음속 노즐에서 수치해석을 수행하였다. 수치해석 검증에서 SST $k-{\omega}$ 난류모델을 사용하여 실험결과를 잘 구현하였다. 광범위한 노즐 압력비와 분사 압력비에서 편향각도, 시스템의 전체 추력비 및 추력 효율을 조사하였다. 본 연구에서 이중목 노즐의 추력벡터제어 시스템의 성능 변화는 2차원 계산영역에서 명확하게 설명되었다. 본 연구에서 얻어진 결과들은 유체추력벡터제어 분야에 중요한 기초자료를 제공할 것이다.

Keywords

References

  1. Mason, M.S. and Crowther, W.J., "Fluidic Thrust Vectoring for Low Observable Air Vehicles," 2nd AIAA Flow Control Conference, O.R., USA, AIAA 2007-5084, 2004.
  2. Asbury, S.C. and Capone, F.J., "High-alpha Vectoring Characteristics of the F-18/HARV," Journal of Propulsion and Power, Vol. 10, No. 1, pp. 116-121, 1994. https://doi.org/10.2514/3.23719
  3. Henderson, W.P., "Propulsion System Integration in High Performance Aircraft," Journal of Aerospace Engineering, Vol. 10, pp. 21-25, 1990.
  4. Herbst, W.B., "Future Fighter Technologies," Journal of Aircraft, Vol. 17, No. 8, pp. 561-566, 1980. https://doi.org/10.2514/3.44674
  5. Chambers, J.R., "High-alpha Flight Dynamics: Lessons Learned," 4th Applied Aerodynamics Conference, Fluid Dynamics and Co-Located Conference, S.D., AIAA 86-1774-CP, 1986.
  6. Deng, R.Y., Kong, F.S. and Kim, H.D., "Numerical Simulation of Fluidic Thrust Vectoring in an Axisymmetric Supersonic Nozzle," Journal of Mechanical Science and Technology, Vol. 28, No. 12, pp. 4979-4987, 2014. https://doi.org/10.1007/s12206-014-1119-x
  7. Deng, R.Y. and Kim, H.D., "A Study on the Thrust Vector Control Using a Bypass Flow Passage," Proceeding of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 229, No. 9, pp. 1722-1729, 2015. https://doi.org/10.1177/0954410014558693
  8. Deere, K.A., "Summary of Fluidic Thrust Vectoring Research Conducted at NASA Langley Research Center," 21th AIAA Applied Aerodynamics Conference, O.R., AIAA 2003-3800, 2003.
  9. Wu, K.X., Kim, H.D. and Jin, Y.Z., "Fluidic Thrust Vector Control Based on Counter-Flow Concept," Proceeding of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, pp. 1-11, 2018.
  10. Deere, K.A., Berrier, B.L., Flamm, J.D. and Johnson, S.K., "Computational Study of Fluidic Thrust Vectoring Using Separation Control in a Nozzle," 21st AIAA Applied Aerodynamics Conference, Fluid Dynamics and Co-Located Conference, O.R., USA, AIAA 2003-3803, 2003.
  11. Flamm, J.D., Deere, K.A., Berrier, B.L. and Johnson, S.K., "Design Enhancements of the Two-Dimensional, Dual Throat Fluidic Thrust Vectoring Nozzle Concept," 3rd AIAA Flow Control Conference, S.F., USA, AIAA 2006-3701, 2006.
  12. Shi, J.W., Zhou, L., Wang, Z.X. and Sun, X.L., "Investigation on Flowfield Characteristics and Performance of Shock Vector Control Nozzle Based on Confined Transverse Injection," Journal of Engineering for Gas Turbines and Power, Vol. 138, No. 101502, pp. 1-11, 2016.