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Numerical Heat Transfer, Part A: Applications
An International Journal of Computation and Methodology
Volume 79, 2021 - Issue 5
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Original Articles

Evaluation of breakup models for liquid side jets in supersonic cross flows

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Pages 353-369 | Received 09 Oct 2020, Accepted 03 Nov 2020, Published online: 18 Nov 2020

References

  • K. C. Lin, P. Kennedy and T. Jackson, “Penetration heights of liquid jets in high-speed crossflows,” 40th AIAA Aerospace Sciences Meeting & Exhibit, Jan 2002. p. 873. DOI: 10.2514/6.2002-873.
  • K. C. Lin, P. Kennedy and T. Jackson, “Structures of Water Jets in a Mach 1.94 Supersonic Crossflow,” 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 2004. AIAA. DOI: 10.2514/6.2004-971.
  • W. M. VanLerberghe, J. G. Santiago, J. C. Dutton and R. P. Lucht, “Mixing of a sonic transverse jet injected into a supersonic flow,” AIAA J., vol. 38, no. 3, pp. 470–479, 2000.
  • J. C. McDaniel and J. Graves Jr, “Laser-induced-fluorescence visualization of transverse gaseous injection in a nonreacting supersonic combustor,” J. Propulsion Power, vol. 4, no. 6, pp. 591–597, 1988. DOI: 10.2514/3.23105.
  • B. K. McMillin, J. M. Seitzman and R. K. Hanson, “Comparison of NO and OH planar fluorescence temperature measurements in scramjet model flowfield,” AIAA J., vol. 32, no. 10, pp. 1945–1952, 1994.
  • A. Ben-Yakar, M. G. Mungal and R. K. Hanson, “Time evolution and mixing characteristics of hydrogen and ethylene transverse jets in supersonic crossflows,” Phys. Fluids, vol. 18, no. 2, pp. 026101, 2006. DOI: 10.1063/1.2139684.
  • A. Rothstein and P. Wantuck, “A study of the normal injection of hydrogen into a heated supersonicflow using planar laser-induced fluorescence,” 28th Joint Propulsion Conference and Exhibit, 1992, p. 3423. DOI: 10.2514/6.1992-3423.
  • S. H. Smith and M. G. Mungal, “Mixing, structure and scaling of the jet in crossflow,” J. Fluid Mech., vol. 357, pp. 83–122, 1998. DOI: 10.1017/S0022112097007891.
  • M. R. Gruber, A. S. Nejad, T. H. Chen and J. C. Dutton, “Mixing and penetration studies of sonic jets in a Mach 2 freestream,” J. Propulsion Power, vol. 11, no. 2, pp. 315–323, March-April 1995.
  • M. R. Gruber, A. S. Nejad, T. H. Chen and J. C. Dutton, “Compressibility effects in supersonic transverse injection flowfields,” Physics Fluids, vol. 9, no. 5, pp. 1448–1461, 1997. DOI: 10.1063/1.869257.
  • M. R. Gruber, A. S. Nejad, T. H. Chen and J. C. Dutton, “Transverse Injection from Circular and Elliptic Nozzles into a Supersonic Crossflow,” j. Propulsion Power, vol. 16, no. 3, pp. 449–457, May-June 2000.
  • P. J. O'Rourke and A. A. Amsden. The TAB method for numerical calculation of spray droplet breakup. SAE Technical Paper No. 872089, 1987.
  • M. A. Patterson and R. D. Reitz, “Modeling the effects of fuel spray characteristics on diesel engine combustion and emission,” SAE Trans., vol. 107, pp. 27–43, 1998.
  • A. B. Liu, D. Mather and R. D. Reitz, “Modeling the effects of drop drag and breakup on fuel sprays,” SAE Trans., vol. 102, no. 3, pp. 83–95, 1993.
  • P. Li, Z. Wang, M. Sun and H. Wang, “Numerical simulation of the gas-liquid interaction of a liquid jet in supersonic crossflow,” Acta Astronautica, vol. 134, pp. 333–344, May 2017.
  • S. C. Kong, P. K. Senecal and R. D. Reitz, “Developments in spray modeling in diesel and direct-injection gasoline engines,” Oil Gas Sci. Technol., vol. 54, no. 2, pp. 197–204, 1999.
  • Y. Li and S. C. Kong, “Mesh refinement algorithms in an unstructured solver for multiphase flow simulation using discrete particles,” J. Computational Phys., vol. 228, no. 17, pp. 6349–6360, 2009. DOI: 10.1016/j.jcp.2009.05.018.
  • R. Kolakaluri, Y. Li and S. C. Kong, “A unified spray model for engine spray simulation using dynamic mesh refinement,” Int. J. Multiphase Flow, vol. 36, no. 11-12, pp. 858–869, 2010. DOI: 10.1016/j.ijmultiphaseflow.2010.08.001.
  • X. Fan, J. Wang, F. Zhao, J. Li and T. Yang, “Eulerian–Lagrangian method for liquid jet atomization in supersonic crossflow using statistical injection model,” Adv. Mech. Eng., vol. 10, no. 2, pp. 168781401876129, 2018. DOI: 10.1177/1687814018761295.
  • S. Arunajatesan, “Evaluation of Two-Equations RANS Models for Simulation of Jet-in-Crossflow Problems,” In 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 2012, p. 1199). DOI: 10.2514/6.2012-1199.
  • S. Arunajatesan and M. A. McWherter-Payne, “Unsteady modeling of jet-in-crossflow problems,” 43rd AIAA Fluid Dynamics Conference, 2013, p. 3099). DOI: 10.2514/6.2013-3099.
  • S. J. Beresh, J. F. Henfling, R. J. Erven and R. W. Spillers, “Penetration of a transverse supersonic jet into a subsonic compressible crossflow,” AIAA J., vol. 43, no. 2, pp. 379–389, 2005. DOI: 10.2514/1.9919.
  • C. J. Tam, R. Baurle and M. Gruber, “Numerical study of jet injection into a supersonic crossflow,” 35th Joint Propulsion Conference and Exhibit, Los Angeles, CA, U.S.A, 1999, p. 2254. AIAA. DOI: 10.2514/6.1999-2254.
  • C. Schaupp and R. Friedrich, “Large-eddy simulation of a plane reacting jet transversely injected into supersonic turbulent channel flow,” Int. J. Comput. Fluid Dynamics, vol. 24, no. 10, pp. 407–433, 2010. DOI: 10.1080/10618562.2010.533121.
  • J. A. Boles, J. R. Edwards and R. A. Bauerle, “Large-Eddy/Reynolds-Averaged Navier-Stokes Simulations of Sonic Injection into Mach 2 Crossflow,” AIAA J., vol. 48, no. 7, pp. 1444–1456, 2010. DOI: 10.2514/1.J050066.
  • S. Kawai and S. Lele, “Mechanisms of jet mixing in a supersonic crossflow: A study using large-eddy simulation,” 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, 2008, p. 4575. AIAA. DOI: 10.2514/6.2008-4575.
  • S. Kawai and S. Lele, “Large-Eddy Simulation of Jet Mixing in a Supersonic Turbulent Crossflow,” 19th AIAA Computational Fluid Dynamics, San Antonio, Texas, 2009, p. 3795. AIAA. DOI: 10.2514/6.2009-3795.
  • S. Kawai and S. K. Lele, “Large-eddy simulation of jet mixing in supersonic crossflows,” AIAA J., vol. 48, no. 9, pp. 2063–2083, 2010. DOI: 10.2514/1.J050282.
  • B. Van Leer, 1976. MUSCL, a new approach to numerical gas dynamics. Computing in Plasma Physics and Astrophysics.
  • P. L. Roe, “Approximate Riemann solvers, parameter vectors, and difference schemes,” J. Comput. Phys., vol. 43, no. 2, pp. 357–372, 1981.
  • T. Siikonen, “An application of Roe's flux‐difference splitting for k‐ϵ turbulence model,” Int. J. Numer. Meth. Fluids, vol. 21, no. 11, pp. 1017–1039, 1995.
  • C. T. Crowe, J. D. Schwarzkopf, M. Sommerfeld and Y. Tsuji, 2011, Multiphase flows with droplets and particles. CRC Press.
  • J. Sauter, 1926. “Determining size of drops in fuel mixture of internal combustion engines.” NACA Technical Memorandums No. 390.

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