MEASUREMENTS AND PREDICTIONS OF A LIQUID SPRAY FROM AN AIR-ASSIST NOZZLE
Author(s) -
Daniel L. Bulzan,
Y. Levy,
Suresh K. Aggarwal,
S. Chitre
Publication year - 1992
Publication title -
atomization and sprays
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.418
H-Index - 52
eISSN - 1936-2684
pISSN - 1044-5110
DOI - 10.1615/atomizspr.v2.i4.50
Subject(s) - nozzle , sauter mean diameter , materials science , mechanics , spray nozzle , micrometer , particle (ecology) , analytical chemistry (journal) , thermodynamics , optics , chemistry , chromatography , physics , oceanography , geology
Droplet size and velocity and gas velocity were measured in a water spray using a twocomponent Phase/Doppler Particle Analyzer. A complete set of measurements was obtained at axial locations from 5 to 50 cm downstream of the nozzle. The nozzle used was a simple axisymmetric air-assist nozzle. The sprays produced, using the atomizer, were extremely fine. Sauter mean diameters were less than 20 _m at all locations. Measurements were obtained for droplets ranging from l to 50 /._. The gas phase was seeded with micron sized droplets, and droplets having diameters of 1.4 _ and less were used to represent gas-phase properties. _easurements were compared with predictions from a multi-phase computer model. Initial conditions for the model were taken from measurements at 5 cmdownstream. Predictions for both the gas phase and the droplets showed relatively good agreement with the measurements. Nomenclature a acceleration of gravity Ci Cd constants in turbulence model drag coefficient d nozzle diameter dp k droplet diameter turbulence kinetic energy Le dissipation length scale of eddy mp droplet mass n number of droplet groups n i number of droplets per unit time in group i Re Reynolds number r radial distance *Aerospace Engineer, member AIAA. *'NRC Research Associate, on leave from Technion, Israel Institute of Technology, Haifa, Israel_ member AIAA. Associate professor, Dept. of Mechanical Engineering, member AIAA. _'Graduate student, Dept. of Mechanical Engineering. S source term Sp source term due to droplets t time t e eddy lifetime u axial velocity Vj volume of computational cell ) v radial velocity w angular velocity x axial distance Xp droplet position vector e rate of dissipation of turbulence kinetic energy p viscosity _t turbulent viscosity p density _i turbulent Prandtl/Schmidt number 0 generic property qXp relative path length of droplets in an eddy Vtp droplet residence time in an eddy Subscri_: c centerIine quantity o initial axial location p droplet property = ambient condition Superscripts: ( )' fluctuating quantity (-) time averaged value (*) vector quantity (~) Favre averaged value Copyright © 1990 by the American Institute of Aeronautics and Astronautics, Inc. No copyright is asserted in the United States under Title 17, U.S. Code. The U.S. Government has a royalty-free license to exercise all rights under the copyright claimed herein for Governmental purposes. All other rights are re_rved by the copyright owner.
Accelerating Research
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom
Address
John Eccles HouseRobert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom