DOI QR코드

DOI QR Code

Design Study on the Flow Characteristics of a Gas Management System for a Vertical Launching System

함정 수직발사대 화염처리장치 형상에 따른 유동특성 연구

  • Received : 2013.03.08
  • Accepted : 2013.08.16
  • Published : 2013.10.05

Abstract

The gas management system for a vertical launching system must be safely managed within a ship. The plenum and uptake are capable of containing and surviving a full-burning restrained firing without loss of gas management integrity. To secure the safety, the pressure characteristics with a supersonic under-expanded jet on a gas management system are numerically investigated using computational fluid dynamics. The results of present analysis and the preliminary design of the gas management system are described in this paper.

Keywords

References

  1. Yagla, J. J. and Anderson, L. P. Jr., "Internal Ballistics and Missile Launch Environment for the Vertical Launching System", AIAA and ASME, Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference, 3rd, St. Louis, MO, June 7-11, 1982.
  2. York, B. J., Sinha, N., Dash, S. M., Anderson, L. and Gominho, L., "Navier-Stokes Simulation of Plume/Vertical Launching System Interaction Flow Fields", AIAA, Aerospace Sciences Meeting and Exhibit, 30th, Reno, NV, Jan. 6-9, 1992.
  3. Lee, K. S. and Hong, S. K., "Supersonic Jet Impingement Navier-Stokes Computations for Vertical Launching System Design Applications", Journal of Spacecraft and Rockets, Vol. 41, No. 5, pp. 735-744, 2004. https://doi.org/10.2514/1.13077
  4. 홍승규, 이광섭, 성웅제, "초음속 노즐과 벽면 충돌제트의 유동특성", 한국군사과학기술학회지, 제4권, 제2호, pp. 256-262, 2001.
  5. Miller, M. J., Koo, J. H., Siebenshuh, J. R., Wilson, D. and Beckley, D., "Development of a Scaled Ducted Launcher for Ablative Testing", AIAA, Aerospace Sciences Meeting and Exhibit, 33rd, Reno, NV, January 9-12, 1995.
  6. Koo, J. H., Ho, D. W. H. and Ezekoye, O. A., "A Review of Numerical and Experimental Characterization of Thermal Protection Materials- Part I. Numerical Modeling", AIAA/ASME/ASEE, Joint Propulsion Conference and Exhibit, 42nd, Sacramento, California, July 9-12, 2006.
  7. Koo, J. H., Ho, D. W. H., Bruns, M. C. and Ezekoye, O. A., "A Review of Numerical and Experimental Characterization of Thermal Protection Materials-Part II. Properties Characterization", AIAA/ASME/ASEE/AHS/ASC, Structures, Structural Dynamics, and Materials Conference, 48th, Honolulu, Hawaii, April 23-26, 2007.
  8. Ginzberg, I. P., Semilentenko, B. G., Terpigorev, V. S. and Iskov, V. N., "Some Singularities of Supersonic Underexpanded Jet Interaction with a Plane Obstacle", Journal of Engineering Physics, Vol. 19, pp. 1081-1084, 1973.
  9. Kalghatgi, G. T. and Hunt, B. L., "The Occurrence of Stagnation Bubbles in Supersonic Jet Impingement Flows", Aeronautical Quarterly, Vol. 27, pp. 169-185, 1976. https://doi.org/10.1017/S0001925900007678
  10. Inman, J. A., Danehy, P. M., Nowak, R. J. and Alderfer, D. W., "The Effect of Impingement on Transitional Behavior in Underexpanded Jets", AIAA, Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, 47th, Orlando, Florida, January 5-8, 2009.
  11. Lee, K. S., Lee, J. G., Hong, S. K. and Ahan, C. S., "Numerical Simulations of the Supersonic Jet Impingement in a Confined Plenum of Vertical Launching System", Korea Society for Computational Fluids Engineering Parallel CFD 2006, pp. 301-305, 2006.
  12. 2011, ESI CFD, Inc., CFD-FASTRAN User's Manual-Version 2011, Cummings Research Park, pp. 97-125, 2011.