Visual characteristics and initial growth rates of round cryogenic jets at subcritical and supercritical pressures

Cryogenic liquids initially at a subcritical temperature were injected through a round tube into an environment at a supercritical temperature and at various pressures ranging from subcritical to supercritical values. Pure N2 and O2 were injected into environments composed of N2, He, Ar, and various mixtures of CO+N2. The results were photographically observed and documented near the exit region using a CCD camera illuminated by a short duration backlit strobe light. At low subcritical chamber pressures, the jets showed surface irregularities that amplified downstream, exhibiting intact, shiny, but wavy (sinuous) surface features that eventually broke up into irregularly shaped small entities. A further increase of chamber pressure at constant jet initial and ambient temperatures caused the formation of many small droplets to be ejected from the surface of the jet similar to what is observed in the second wind-induced jet breakup regime. As the chamber pressure was further increased, the transition to a f...

[1]  A. Roshko,et al.  The compressible turbulent shear layer: an experimental study , 1988, Journal of Fluid Mechanics.

[2]  C. Schweitzer,et al.  Injection and Mixing Processes in High Pressure LOX/GH2 Rocket Combustors. , 1996 .

[3]  A. Roshko,et al.  On density effects and large structure in turbulent mixing layers , 1974, Journal of Fluid Mechanics.

[4]  E. John List,et al.  Investigations of round vertical turbulent buoyant jets , 1988, Journal of Fluid Mechanics.

[5]  D. Talley,et al.  Raman imaging of transcritical cryogenic propellants , 1996 .

[6]  Gerard M. Faeth,et al.  Structure and atomization properties of dense turbulent sprays , 1991 .

[7]  J. Bellan,et al.  Isolated fluid oxygen drop behavior in fluid hydrogen at rocket chamber pressures , 1998 .

[8]  G. N. Abramovich The Theory of Turbulent Jets , 2003 .

[9]  H. Schlichting Boundary Layer Theory , 1955 .

[10]  B. Chehroudi,et al.  Initial Growth Rate and Visual Characteristics of a Round Jet into a Sub- to Supercritical Environment of Relevance to Rocket, Gas Turbine, and Diesel Engines , 1999 .

[11]  G. Faeth,et al.  Bipropellant droplet combustion in the vicinity of the critical point , 1971 .

[12]  R. Reitz,et al.  On the Dependence of Spray Angle and Other Spray Parameters on Nozzle Design and Operating Conditions , 1979 .

[13]  P. Dimotakis Two-dimensional shear-layer entrainment , 1986 .

[14]  Wolfgang Rodi,et al.  Vertical turbulent buoyant jets : a review of experimental data , 1980 .

[15]  B. Ivancic,et al.  Propellant Atomization in LOX/GH2 Rocket Combustors. , 1998 .

[16]  C. Richards,et al.  Global density effects on the self-preservation behaviour of turbulent free jets , 1993, Journal of Fluid Mechanics.

[17]  Frediano V. Bracco,et al.  On the Intact Core of Full-Cone Sprays , 1985 .

[18]  J. Naber,et al.  Effects of Gas Density and Vaporization on Penetration and Dispersion of Diesel Sprays , 1996 .

[19]  J. A. Newman,et al.  Behavior of a Liquid Jet near the Thermodynamic Critical Region , 1971 .

[20]  D. W. Bogdanoff,et al.  Compressibility Effects in Turbulent Shear Layers , 1983 .

[21]  G. L. Brown,et al.  A small, Fast-Response Probe to Measure Composition of a Binary Gas Mixture , 1972 .