The Theory of Turbulent Jets

By G. N. Abramovich. 2003

912 citations recorded by the source corpus.

This chapter contains sections titled: Fundamental Concepts, Submerged Jet, Velocity Profiles in a Submerged Jet, Spread of a Turbulent Submerged Jet, Lines of Constant Velocity in a Submerged Jet, Velocity Variation Along the Axis of a Submerged Jet, Heat Transfer in a Submerged Jet, Diffusion of Constituents in a Submerged Jet, Velocity, Temperature, and Concentration Profiles in a Turbulent Jet Spreading into an External Stream of Fluid, Spread of a Turbulent Jet into a Coflowing or Counterflowing External Stream, Turbulence Characteristics in a Free Jet

Subfields: Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/d3c5fb825cb85661e5c24c4a42d6a306fb018e48

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In Computational Mechanics

Citations in the corpus

Integral Model for Turbulent Buoyant Jets in Unbounded Stratified Flows. Part I: Single Round Jet (2004, background): “for the pure jet in stagnant ambient by Abramovich [44], or for the vertically rising pure plume by Lee and Jirka [45].”
INJECTION OF FLUIDS INTO SUPERCRITICAL ENVIRONMENTS (2006, methodology): “According to Abramovich (1963), the length of the potential core in isothermal uniform density axisymmetric and two-dimensional jets is estimated to be about 6 to 10 injector diameters; whereas for non-isothermal cold jets injected into hot environments, it can reach up to about 25 injector…”
Transverse jets and jet flames. Part 1. Scaling laws for strong transverse jets (2001, background): “We note that Abramovich (1963) assumes that jet width is proportional to jet arc length (as opposed to wall-normal distance), which matches the data in the slightly deflected region reasonably well, but poorly matches the far-field data, where the jet is nearly parallel to the crossflow.”
Free underexpanded jets in a quiescent medium: A review (2015, background): “On the contrary, the steady state of the flow has been largely studied in the past [3, 4, 5, 16, 22, 23, 28, 59, 62, 64, 69, 81, 87, 104, 106, 145, 152, 165, 164, 193, 194, 210, 211, 212, 225, 226, 252], since it corresponded to the most often encountered situations.”
Recent Experimental Efforts on High-Pressure Supercritical Injection for Liquid Rockets and Their Implications (2012, methodology): “According to Abramovich [14], the length of the “potential core” in isothermal uniform-density axisymmetric and two-dimensional jets is estimated to be about 6 to 10 injector diameters; whereas for nonisothermal cold jets injected into hot environments, it can reach up to about 25 injector diameters”
Wind turbine wake aerodynamics (2003, methodology): “[217] used velocity profiles obtained from models on co-flowing jets by Abramovich [218].”