Piloted Turbulent flame
Code name: | pf03 |
Wind Tunnel Dimension (m): | 0.305 * 0.305 |
Burner Diameter (m) ID and OD: | 0.0072 and 0.0076 |
Pilot annulus (m) ID and OD: | 0.0180 and 0.0190 |
Fuel mixture: | CH3OH-AIR=50.0%-50.0% (by vol.) |
Stoichiometric Mixture Fraction: | 0.2560 |
Blowoff velocity (m/s): | 160.0 |
Pilot gas mixture: | C2H2-H2-CO2-AIR=3.6-24.8-7.3-64.3 (%by vol) |
Pilot Stoichiometric Mixture Fraction: | 0.2 |
Pilot unburnt bulk velocity(m/s): | 2.1 |
Coflow air velocity (m/s): | 15 |
Open flame, no enclosure |
The following values have been used in calculating the
mixture fraction:
Total Mass fraction of Oxygen atoms in the air stream, Zo,o =
0.233
Total Mass fraction of Carbon atoms in the air stream, Zc,o =
0.0
Total Mass fraction of Hydrogen atoms in the air stream, Zh,o = 0.0
Total Mass fraction of Oxygen atoms in the fuel stream, Zo,f =
0.3733
Total Mass fraction of Carbon atoms in the fuel stream, Zc,f =
0.1970
Total Mass fraction of Hydrogen atoms in the fuel stream, Zh,f = 0.0662
Data files provided for this fuel mixture: (to download the files click here)
Jet velocity Axial location Radial Location
OUR REF. Filenames
(m/s)
(x/D) (mm)
--------------------------------------------------------------------------
104.8
15
6 M1AOUT.407 pf03s15.01
104.8
15
6 M1AOUT.408
pf03s15.02
104.8
15
8 M1AOUT.404
pf03s15.03
104.8
15
8 M1AOUT.405
pf03s15.04
104.8
15
8 M1AOUT.406
pf03s15.05
131.0
15
6 M1AOUT.409
pf03t15.01
131.0
15
8 M1AOUT.410
pf03t15.02
131.0
15
8 M1AOUT.411
pf03t15.03
156.4
15
8 M1AOUT.412
pf03v15.01
156.4
15
8 M1AOUT.413
pf03v15.02
145.7
15
8 M1AOUT.414
pf03x15.01
145.7
15
8 M1AOUT.415
pf03x15.02
145.7
15
8 M1AOUT.416
pf03x15.03
151.5
15
8 M1AOUT.417
pf03y15.01
151.5
15
8 M1AOUT.418
pf03y15.02
151.5
15
8 M1AOUT.419
pf03y15.03
© 2002-10 The University of Sydney. Last updated: 1 Sept 2010
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