Axisymmetric Bluff Body Turbulent Flow

 

Code name: B1F1
Wind Tunnel Dimension (m): 0.305 * 0.305
Coflow air shroud (m): 0.086 ID, 0.090 OD
Jet Diameter (m): 0.0020
Bluff Body Diameter (m): 0.0380
Fuel mixture: CH4 = 100% (by vol.)
Stoichiometric Mixture Fraction: 0.0550
Blowoff velocity (m/s): 67.0
Shroud air velocity (m/s): 15
Wind tunnel air velocity (m/s): 2
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 = 0.0
Total Mass fraction of Carbon   atoms in the fuel stream, Zc,f = 0.7485
Total Mass fraction of Hydrogen atoms in the fuel stream, Zh,f = 0.2515

NOTE: The data presented for this flame should be used with care as
      they are affected by fluorescence  interferences from soot
      precursors as well as other species.
 
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)          
-----------------------------------------------------------------------------
   46.6            2.0            12&13        B2M70D76RES.29204  b1f1s02.01
   46.6            2.0            9&10          B2M70D76RES.29205  b1f1s02.02
 

DISCLAIMER: No responsibility is assumed by the suppliers of this data for any injury and/or property damage as a matter of products liability, negligence or otherwise, or from any use or operation of any methods, products, instructions, or ideas based on these data.