VMFRT005

VMFRT005
Engine Combustion Network Reacting Flow Case jkldaAL4

Overview

ReferenceRetrieved from Engine Combustion Network data search utility: https://ecn.sandia.gov/ecn-data-search/ Accessed on April 7, 2020.

Find relevant data and information by choosing the parameters highlighted in gray below on the ECN data search utility.

SolverAnsys Forte
Physics/Models Engine Combustion Network (ECN) Nonreacting Flow Case jkldaAL4
Input FilesP_150MPa_R.ftsim
Project FilesLink to Project Files Download Page

Test Case

This test recreates the Engine Combustion Network (ECN) Spray A target case characterized by high-pressure liquid fuel injection in conditions relevant to diesel engines. In this case, the combustion chamber has a cubical shape (length = 10.8 cm), the oxygen content is 15%, and the difference between the fuel injector pressure and ambient gas pressure is 150 MPa. The fuel entering the combustion chamber through the spray injector is n-dodecane (nC12).

The model includes two refined regions of respectively 2 mm and 1 mm around the jet. The table below lists the setup parameters for the experiment and simulation. No liquid penetration length measurements were found on the ECN repository for this case, but experimental data for the vapor penetration length can be found on the ECN site in the form of a text file:

The modeling prediction for vapor penetration length is compared with the experimental results including error bars in Figure 206: Vapor and liquid penetration length. Additional measurements on the ECN data search utility report the lift-off length measurement and the ignition delay time. The slight overprediction is likely due to imperfections in the low temperature chemical kinetics of the reacting fuel and air mixture.

Test case properties
PinjMinjDurationinjVambρambCompositionambPambTambTfuelDnozzle
150 MPa14 mg6 ms20 cm/s22.8 kg/m3

N2 = 75.15%

CO2 = 6.22%

H2O = 3.62%

O2 = 15.00%
5.94 MPa900 K373 K0.084 mm
Simulation Settings
RTdistvinj profileSpray initialization modelL/DR/DSAM on ∇T∇Vel∇Y*[a]Turbulence modelMesh sizeMAXdtinitial
2.2FlatNozzle flow11.90.2380.5 mmRANS RNG-ke4 mm1E-7 s

[a] Y*=Fuel Vapor Mass Fraction

Results Comparison for Ansys Forte

Figure 206: Vapor and liquid penetration length

Vapor and liquid penetration length

 

TargetPredicted
Lift-off length
16.7 mm18.0 mm
Ignition delay time
0.41 ms0.7 ms