Distributions across the plume of transverse liquid and slurry jets in supersonic airflow

Liquid and slurry jets were injected through a circular orifice transverse to a M = 3 airflow. Mass samples of both jets were taken across the plume 30 injector diameters downstream. Pitot and static pressure surveys were taken across the liquid jet. These data allowed the calculation across the liquid jet plume of the Mach number, air mass flow, liquid-to-air ratio, and momentum flux. In the center third of the plume area, there is a core region of subsonic airflow that carries two-thirds of the mass collected in the plume. In the core, the liquid mass flow is nearly constant from side to side at a given height and the average velocity of the liquid is only 30-60% of the local air velocity. A supersonic mixing region surrounds the core region. Comparison with these direct sampling results indicate that correlations developed from photography are inadequate in determining the penetration and width of either jet. The slurry jet showed substantial phase separation. When a 30% mass-loaded slurry of 1-5 p,m silicon dioxide particles mixed with water was injected, the local loading varied from a low of 13% at the bottom of the plume to 100% outside the plume.

[1]  J. Schetz,et al.  Effects of properties and location in the plume on droplet diameter for injection in a supersonic stream , 1983 .

[2]  J. Schetz,et al.  Penetration and breakup of slurry jets in a supersonic stream , 1983 .

[3]  M. Yang,et al.  Trajectory with diffusion method for predicting the fuel distribution in a transverse stream , 1983 .

[4]  Merrill K. King,et al.  Ignition and Combustion of Boron Particles and Clouds , 1982 .

[5]  J. Schetz,et al.  Atomization of Impinging Liquid Jets in a Supersonic Crossflow , 1982 .

[6]  Joseph A. Schetz,et al.  Wave phenomena in liquid jet breakup in a supersonic crossflow , 1980 .

[7]  J. Schetz,et al.  Effect of Injector Shape on Penetration and Spread of Liquid Jets , 1975 .

[8]  A. Jakubowski,et al.  Effect of Injector Geometry on Penetration, Spread and Structure of a Liquid Jet Injected Normal to a Supersonic Air Stream. , 1973 .

[9]  E. A. Kush,et al.  Liquid Jet Injection into a Supersonic Flow , 1972 .

[10]  K. Horn,et al.  Investigation of injectant properties on jet penetration in a supersonic stream , 1971 .

[11]  R. Edelman,et al.  Combustion of liquid hydrocarbons in a high-speed airstream , 1970 .

[12]  K. Horn,et al.  Study of penetration of a liquid injectant into a supersonic flow. , 1968 .

[13]  I. Catton,et al.  Study of Liquid Jet Penetration in a Hypersonic Stream , 1968 .

[14]  S. Molder,et al.  Secondary liquid injection into a supersonic airstream. , 1966 .

[15]  P. C. Setze,et al.  Some combustion problems of high-energy fuels for aircraft , 1958 .

[16]  W. Olson,et al.  NACA Research on Slurry Fuels Through 1954 , 1955 .