Session: 04-15: Combustor Flows

Paper Number: 80350

80350 - Investigation of Water Films Shed From an Airfoil in a High-Speed Flow 

The breakup of liquid films in high-speed flows are found in many applications.  These include pre-filming air blast atomization found in fuel injectors, and shedding of droplet off of airfoils.  In this work, a test rig has been developed and applied to study the breakup of water films from the trailing edge of an NACA 0012 airfoil placed in a high-speed air flow.  The results provided reflect a new detailed data set focus on air velocities above 75 m/s.  CFD simulation was used to guide the development of the rig and the associated boundary and inlet conditions.  In the present work, air velocities up to 200 m/s were used with water films between 0.36 and 3.6 cm²/s.  The water film was introduced onto one surface through a series of 0.5 mm holes separate by 1mm at a location 35 mm downstream of the leading edge of the vane.  High speed video was used to document the sheet breakup behavior from the edge of the airfoil.  Image analysis was used to identify the breakup length of ligaments formed.  Laser diffraction was used 50 mm downstream of the trailing edge of the vane to determine the droplet size distribution and associated representative average diameters generated.  In addition , phase Doppler interferometry measurements were also made 50 mm downstream of the vane trailing edge to add additional information about the droplet sizes and velocities.  Finally, fluorescence-based imaging was used to quantify relative film thickness at the trailing edge of the vane.  A series of test conditions were run between 50 and 200 m/s using multilevel factorial designed experiments.  The results obtained were subject to analysis of variance to generate correlations for breakup length and droplet representative diameters as a function of the conditions studied.  The analysis was conducted on dimensionless versions of the variables studied to help connect the results to the physics of the situation.  For example, rather than using air velocity to correlation the behavior, the Weber number (based on gas phase density and velocity) was used owing to its historical ability to describe liquid breakup processes.  The results obtained are compared with other studies in the literature and good agreement was found for the conditions at which a comparison could be made.  It is observed that, for the conditions studied, liquid film thickness has little effect on the resulting droplet sizes, especially for the higher air velocity cases studied.  The results also illustrate the sensitivity to choice of characteristic length which has generally consisted of trailing edge geometry or boundary layer thickness.  In contrast, liquid film does influence the ligament breakup length, although the time to breakup is less affected.  Overall the correlations developed provide engineering tools to help estimate ligament and drop size behavior for water films shed from airfoils in a high speed flow.

Presenting Author: Vincent Mc Donell Univ Of California

Presenting Author Biography: Professor McDonell directs combustion research at the UCI Combustion Laboratory at University of California, Irvine.

Authors:

Brandon Esquvias Rodriguez University of California, Irvine
Brendan Hickey University of California, Irvine
Vincent Mc Donell Univ Of California
Sochiro Tabata Mitsubishi Heavy Industries
Shigeki Senoo Mitsubishi Heavy Industries