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Papers : A Study of Numerical Impinging Jet Models for a Like - doublet Injector of Liquid Rockets

논문 : 액체 로켓의 Like - doublet 인젝터의 충돌 제트 수치 모델에 대한 연구


Abstract

기존의 이론적 연구와 실험적 연구를 바탕으로 충돌 제트의 수치 모델을 개발하였다. 본 모델은 like-doublet 충돌제트로부터 생성되는 액적의 모든 특성을 액막이 분열되는 시점에서 결정한다. 액적 특성을 결정하기 위해 이론적 연구로부터 얻어진 액막 두께, 액주의 직경, 액적 크기와 실험적 연구로부터 얻어진 액막/액적 속도, 액막 분열 거리, 분열 주파수, 액적 질량 유량 분포를 이용하였다. 액적의 질량 유량 분포는 Laplace 분포로부터 표준 편차를 이용하여 모사하였다. 또한 실험 결과를 이용하여 액막 분열 거리, 분열 주기, 표준 편차에 대한 경험식을 유도하였다. 개발된 모델은 정성적인 분무 패턴뿐만 아니라 정량적인 SMD 및 질량 유량 분포에서 실험 결과와 잘 일치한다.

Keywords

References

  1. Jeffrey, A. Muss, "Instability Phenomena in Liquid Oxygen/Hydrocarbon Rocket Engines," Liquid Rocket Engine Combustion Instability, edited by V. Yang and W. E. Anderson, Vol 169, Progress in Astronautics and Aeronautics, AIAA, New York, 1994, pp. 73-88.
  2. Taylor, G. I., "Formation of Thin Flat Sheets of Water," Proceedings of the Royal Society of London, A, Vol. 259, 1960, pp. 1-17 https://doi.org/10.1098/rspa.1960.0207
  3. Dombrowski, N. and Hooper P. C., "A Study of the Sprays Formed by Impinging Jets in Laminar and Turbulent Flow," Journal of Fluid Mechanics, Vol. 18, Pt. 3, 1964, pp. 392-400. https://doi.org/10.1017/S0022112064000295
  4. Rangel, R. H. and Sirignano, W. A., "Nonlinear Growth of Kelvin-Helmholtz Instability: Effect of Surface Tension and Density Ratio," Physics of Fluids, Vol. 31, No. 7, 1988, pp. 1845-1855. https://doi.org/10.1063/1.866682
  5. Luigi, D. L. and Michela, C., "Instability of a Spatially Developing Liquid Sheet," Journal of Fluid Mechanics, Vol. 331, 1997, pp. 127-144. https://doi.org/10.1017/S0022112096003916
  6. Xianguo, L. and Tankin, R. S., "On the Temporal Instability of a Two-Dimensional Viscous Liquid Sheet," Journal of Fluid Mechanics, Vol. 226, 1991, pp. 425-443. https://doi.org/10.1017/S0022112091002458
  7. Tang, Y. L. and Schuman, M. D., "Numerical Modeling of Liquid-Liquid Bi-Propellant Droplet/Gas Reacting Flows," AIAA paper 92-0232.
  8. Larosiliere, L., Litchford, R., and Jeng, S., "Hypergolic Bipropellant Spray Combustion and Flow Modeling in Rocket Engines," AIAA paper 90-2238.
  9. Ibrahim, E. A. and Przekwas, A. J., "Impinging Jets Atomization," Physics of Fluids A, Vol. 3, No. 12, 1991, pp. 2981-2987. https://doi.org/10.1063/1.857840
  10. Hasson, D. and Peck, R. E., "Thickness Distribution in a Sheet Formed by impinging Jets," AIChE Journal, Sept. 1964, pp. 752-754. https://doi.org/10.1002/aic.690100533
  11. Dombrowski, N. and Johns, W. R., "The Aerodynamic Instability and Disintegration of Viscous Liquid Sheets," Chemical Engineering Science, Vol. 18, 1963, pp. 203-214. https://doi.org/10.1016/0009-2509(63)85005-8
  12. Squire, H. B., "Investigation of the Instability of a Moving Liquid Film," British Journal of Applied Physics, Vol. 4, 1953, pp. 167-169. https://doi.org/10.1088/0508-3443/4/6/302
  13. Ryan, H. M., Anderson, W. E., Pal, S. and Santoro, R. J., "Atomization Characteristics of Impinging Liquid Jets," Journal of Propulsion and Power, Vol. 11, No. 1, 1995, pp. 135-145. https://doi.org/10.2514/3.23851
  14. Jung, K. H., Park, J. H., Lee, I. S. and Yoon, Y. B., "A Spray Modeling for Uni-Element Like-Doublet Injector of Liquid Rocket Engine," Proceedings of ILASS-Asia, 2001, pp. 111-111.
  15. Clark, C. J. and Dombrowski N., "Aerodynamic instability and disintegration of inviscid liquid sheets," Proceedings of the Royal Society of London, A, Vol. 329, 1972, pp. 467-478. https://doi.org/10.1098/rspa.1972.0124
  16. Anderson, W. E., Ryan H. M. and Santoro, R. J., "Impinging Jet injector Atomization," Liquid Rocket Engine Combustion Instability, edited by V. Yang and W. E. Anderson, Vol 169, Progress in Astronautics and Aeronautics, AIAA, New York, 1994, pp. 215-246.
  17. Lefebvre, A. H., "Drop Size Distributions of Sprays," Atomization and Sprays, 1st ed., Hemisphere, New York, 1989, pp. 79-103.
  18. Amsden, A. A., O' Rourke, P. J., and Butler, T. D., "KIVA-II: A Computer Program for Chemically Reactive Flows with Sprays," Los Alamos National Laboratory, LA-11560-MS, Los Alamos, New Mexico, May. 1989.