A simple hydrodynamic model of a laminar free-surface jet in horizontal or vertical flight

• Published in: Physics of fluids (1994) Vol. 29; no. 8
• Main Authors: Haustein, Herman D., Harnik, Ron S., Rohlfs, Wilko
• Format: Journal Article
• Language: English
• Published: Melville American Institute of Physics 01.08.2017
• Subjects: Computer simulation; Dependence; Emergence; Empirical analysis; Evolution; Flow velocity; Fluid dynamics; Gravitation; Horizontal flight; Impingement; Jet thrust; Mathematical models; Momentum; Nozzles; Physics; Pipe flow; Stagnation; Surface tension; Velocity distribution; Vertical flight; Wettability
• ISSN: 1070-6631; 1089-7666
• DOI: 10.1063/1.4996771

A useable model for laminar free-surface jet evolution during flight, for both horizontal and vertical jets, is developed through joint analytical, experimental, and simulation methods. The jet’s impingement centerline velocity, recently shown to dictate stagnation zone heat transfer, encompasses the entire flow history: from pipe-flow velocity profile development to profile relaxation and jet contraction during flight. While pipe-flow is well-known, an alternative analytic solution is presented for the centerline velocity’s viscous-driven decay. Jet-contraction is subject to influences of surface tension (We), pipe-flow profile development, in-flight viscous dissipation (Re), and gravity (Nj = Re/Fr). The effects of surface tension and emergence momentum flux (jet thrust) are incorporated analytically through a global momentum balance. Though emergence momentum is related to pipe flow development, and empirically linked to nominal pipe flow-length, it can be modified to incorporate low-Re downstream dissipation as well. Jet contraction’s gravity dependence is extended beyond existing uniform-velocity theory to cases of partially and fully developed profiles. The final jet-evolution model relies on three empirical parameters and compares well to present and previous experiments and simulations. Hence, micro-jet flight experiments were conducted to fill-in gaps in the literature: jet contraction under mild gravity-effects, and intermediate Reynolds and Weber numbers (Nj = 5–8, Re = 350–520, We = 2.8–6.2). Furthermore, two-phase direct numerical simulations provided insight beyond the experimental range: Re = 200–1800, short pipes (Z = L/d · Re ≥ 0.01), variable nozzle wettability, and cases of no surface tension and/or gravity.