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UID:0-504@aerospace.technion.ac.il

DTSTART;TZID=Asia/Jerusalem:20160120T163000

DTEND;TZID=Asia/Jerusalem:20160120T173000

DTSTAMP:20230603T192420Z

URL:https://aerospace.technion.ac.il/events/spray-formation-by-homogeneous
 -flash-boiling/

SUMMARY:Spray Formation by Homogeneous Flash Boiling
DESCRIPTION:Lecturer:Moti Levy\n Faculty:Department of Aerospace Engineerin
 g\n Institute:Technion – Israel Institute of Technology\n Location:Class
 room 165\, ground floor\, Library\, Aerospace Eng.\n Zoom: \n Abstract: \n
  Details: \n Injection systems are integrated in a variety of applications
  including fuel injection systems\, painting and coating processes\, medic
 al inhalers and more. In some applications\, and particularly in fuel inje
 ction systems\, the size and size distribution of the droplets are extreme
 ly important properties. For example\, in jet engines and internal combust
 ion engines the droplet's diameter affects the combustion performances\; s
 maller diameter usually means better combustion efficiency and reduced air
  pollution. Additionally\, since even small amount of large droplets incre
 ase the pollutants emission and reduce the efficiency\; the size distribut
 ion is also important. There are various injecting methods to produce a fi
 ne spray that contains small and uniform droplets\; in most of them there 
 is a use of the fluid energy (plane or swirl atomizers)\, an added gas ene
 rgy (air blast and air assist atomizers) or mechanical energy (rotary or s
 linger atomizers) to shatter the liquid jet into fine spray. One of the mo
 re effective methods is to inject the fluid under suitable conditions to a
 ttain flash boiling atomization\; i.e. injecting a pure liquid or a mixtur
 e under initial conditions that ensure an evaporation of the liquid or at 
 least one of the components in a mixture during the rapid depressurization
  caused by the expansion in the orifice. In a binary mixture for example\,
  a high vapor pressure propellant might be dissolved into a low vapor pres
 sure solvent in order to produce rapid evaporation of the propellant durin
 g the depressurization through the orifice\; the rapid evaporation of the 
 propellant disintegrates the solvent into the desired fine spray.\nThe maj
 ority of the studies in this field deal with the most common case in which
  the bubbles are formed in preferred sites on the orifice walls or near co
 ntaminants (heterogeneous nucleation). Studies dealing with homogeneous nu
 cleation\, in which the bubbles are formed in the entire bulk\, are quite 
 rare although finer spays are anticipated since the typical bubble formati
 on rate in the case of homogeneous regime is much higher. The current stud
 y deals with homogeneous flash boiling through a plane orifice. The spray 
 properties of pure liquid and binary mixture were characterized experiment
 ally\, under variety injecting conditions (injecting temperature and press
 ure) and a wide range of propellant mass concentration. Also\, the border 
 line between the two regimes was examined. Additionally\, since the major
 ity of the studies deal with the heterogeneous case\, there are neither su
 itable correlations nor analytical estimations for the typical droplets' d
 iameter under homogeneous nucleation regime. In the current work an analyt
 ical model has been developed to estimate the characteristic droplet diame
 ter in the spray for flash boiling atomization. One significant conclusion
  is that under homogeneous flash boiling\, remarkably small and uniform dr
 oplets are achieved\; therefore by using this relatively simple method ext
 remely fine sprays are obtained comparing to the other methods.
CATEGORIES:Seminars
LOCATION:Classroom 165\, ground floor\, Library\, Aerospace Eng.

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