Primary Atomization (Near Nozzle Flows) Guidance on Experiments and Simulations to be Performed

1. Primary Atomization (Near Nozzle Flows) Guidance on Experiments and Simulations to be Performed SibenduSom: Argonne National Laboratory October 2nd 2014

2. Experimental Objectives • Focus on the near nozzle region within first 10 mm • Concentrate on non-vaporizing experiments • Provide boundary conditions for initializing the simulations for both Spray A and Spray B • Nozzle geometry • Rate of injection • Needle lift & off-axis motion • Injection pressure vs. time • Provide data for validation for both Spray A and Spray B • Liquid mass distribution at nozzle exit and in the spray region • Droplet sizes • Qualitative physics to understand the spray processes • liquid penetration • Assess the uncertainties for all of these parameters

3. Modeling Objectives • Focus on the near nozzle region within first 10 mm • Encourage high-fidelity simulations of fuel sprays to understand the primary atomization physics • Capture the SOI and EOI physics for single and multi-hole injectors • Capture the spray physics during the main injection process for both single and multi-hole injectors • Study the capability of the different modeling approaches (Lagrangian-Eulerian, Eulerian-Eulerian) and CFD frameworks (RANS, LES, DNS) for the simulation of the primary atomization • Assess which physical phenomena are important for including in models: Turbulence, Compressibility, …?

4. Target Injectors • Spray A • Diesel nozzle, single hole, n-dodecane, non-cavitating • High resolution (1 mm) X-ray tomography of Nozzle 675 • Ultra High resolution (0.6 mm) tomography for 678, & 679 • Lift and wobble measured for all nozzles • The target injector will be 675 http://www.sandia.gov/ecn/cvdata/targetCondition/injectorNozGeom.php • Spray B • Diesel nozzle, 3-hole, n-dodecane • .stl files available for 196, 198, 199, 201 • Lift and wobble measured for all the injectors • The target injector will be 201 • Ultra High resolution (0.6 mm) tomography completed and a CFD ready mesh is available http://www.sandia.gov/ecn/cvdata/targetCondition/SpBNozGeo.php

5. Conditions of Interest: Experiments • Spray A and B operating conditions from Argonne: (http://www.sandia.gov/ecn/refs.php?nam=Kastengren-2012-a#Kastengren-2012-a) • Spray A: 675; Spray B: 201 • Priority 1: Pinj = 150 MPa; Priority 2: 100 MPa • Fuel temperature: Spray A - 343 K; Spray B – 338 K • Spray A and Spray B conditions at Sandia and Univ. of Brighton: • Spray A: 675; Spray B: 201 • ?? • ?? • Spray A and Spray B conditions at Chalmers??: • Spray A: 675; Spray B: 201 • ?? • ??

6. Conditions of Interest: Simulations • Spray A and B operating conditions from Argonne: (http://www.sandia.gov/ecn/refs.php?nam=Kastengren-2012-a#Kastengren-2012-a) • Spray A: 675; Spray B: 201 • Priority 1: Pinj = 150 MPa; Priority 2: Pinj = 100 MPa • Fuel temperature: Spray A - 343 K; Spray B – 338 K

7. Anticipated Experimental Results • Microscopic measurements of the initial penetration and spreading angle as the needle opens • Break up and mixing of the sprays at the end of injection at the microscopic level, possible dribble? • USAXS droplet sizing and perhaps optically measured droplet size as well • X-ray radiography of Spray A and Spray B nozzles and plumes of interest • Ballistic imaging of near-nozzle region

8. Data Needed from Experiments • For both Spray A and Spray B injectors: • Mass flow rate at the nozzle exit from virtual ROI tool from CMT and measured nozzle coefficients (already available from ECN3) • Fuel spray penetration vs. time from long-distance microscopy and diffused back-illumination • Contour plots of projected liquid density at 0.1 ms and 0.5 msfrom Argonne • Transverse mass distribution (projected density across the spray) profiles averaged between 0.5 – 1.0 ms: • x = 0.1, 0.6, 2, 6, and 10 mm downstream to nozzle exit • Projection plane is 0°plane (i.e., plane containing fuel inlet, or projection along the z-axis with the injector in the theta = 0 position) • Liquid volume fraction (LVF) across cross-section at x = 0.1, 0.6, 2, 6, 10 mm • the y-axis cut plane • Transverse integrated mass (TIM) vs. axial distance @ 0.5 ms • Mean droplet size (SMD) at x = 1, 4, 8 mm at 0.5 ms after SOI • Mean SMD at the above axial positions vs. axial position

9. Data Needed from Spray A Simulations • Mass flow rate at the nozzle exit • Fuel spray penetration vs. time (0.1% liquid mass fraction) • Contour plots of projected density in the 0°plane at 0.1 and 0.5 ms after actual SOI • Transverse mass distribution (projected density across the spray) in ug/mm2@ x = 0.1, 0.6, 2, 6, and 10 mm downstream to nozzle exit: • between 0.5 – 1.0 ms after SOI, at intervals of 0.1 ms • Averaged profiles between 0.5-1.0 ms at the above locations • 2D contours of LVF at x = 0.1, 0.6, 2, 6, 10 mm at 0.5, 0.75, and 1.0 ms • Transverse integrated mass profiles at 0.5 ms after SOI: • x = 0.1 mm, 0.6 mm, 2 mm, 6 mm, and 10 mm • Mean droplet size (SMD) at x = 1, 4, 8 mm at 0.5 ms after SOI • Mean SMD at the above axial positions vs. axial position • Distributions of SMD vs. radial position at the above axial positions • Dynamics: peak projected density and Full Width Half Maximum (FWHM) of distribution at x = 0.1, 2, 6 mm from nozzle for entire duration of the injection event (in intervals of 20 μs) Set-up conditions from Argonne

10. Data Needed from Spray B Simulations • Spray B target injector (201): • Compare results between different plumes for condition # 1 • Penetration vs. time • Transverse mass distribution at 0.1 mm, 2 mm, and 6 mm • Mean SMD at 1, 4 mm at 0.5 ms after SOI vs. axial position • For plume # 3 which is measured at Argonne • Contour plots of projected density in the 0°plane at 0.1 and 0.5 ms • Transverse mass distribution (projected density across the spray) in ug/mm2@ x = 0.1, 0.6, 2, 6, and 10 mm downstream to nozzle exit: • between 0.5 – 1.0 ms after SOI, at intervals of 0.1 ms • Averaged profiles between 0.5-1.0 ms at the above locations • 2D contours of LVF at x = 0.1, 0.6, 2, 6, 10 mm at 0.5, 0.75, 1.0 ms • Transverse integrated mass profiles at 0.5 ms after SOI: • x = 0.1 mm, 0.6 mm, 2 mm, 6 mm, and 10 mm • Mean droplet size (SMD) at x = 1, 4, 8 mm at 0.5 ms after SOI • Mean SMD at the above axial positions vs. axial position • Distributions of SMD vs. radial position at the above axial positions Set-up conditions from Argonne

11. Confirmed Participants and Volunteers • Experiments • Argonne, Sandia, Univ. of Brighton • Confirm participation: Chalmers • Simulations • Argonne + Univ. of Perugia, ASU, Aachen, Sandia, CMT, GATECH • Confirm participation: UMass, IFPEN, Coria • Possible volunteers • Experiments: ?? • Simulations: ??