**** DATA FROM JOURNAL ARTICLE: Effect of Velocity Ratio on Plane Mixing **
**** Layer Development: Influence of the Splitter Plate Wake by ****
**** R.D. Mehta, Experiments in Fluids, Vol. 10, 1991 ****

Streamwise Development of Velocity Defect.
X (cm)
(U[L]min[LX]-U[L]2[LX])/U[L]0[LX]
 $OPTIONS
 ORIENT ='LANDSCAPE',
 STYLE='TIMESROMAN',
 LINE = 'SYMBOLS',SYMBOL=0,
 YMIN=0.0,YMAX=-1.5,
 WIDTH=3.75,HEIGHT=3.75,
 FIT='TIGHT',
 LEGEND = 'r = 0.5'
 XCOL = 1, YCOL = 2
 $END
11.6   -.047
31.9  -.01
72.6  -.009
110.7  -.006
143.7  -.01
204.6  -.003
236.1  -.008
266.5  -0.0
END CURVE
 $OPTIONS
 LINE = 'SYMBOLS',SYMBOL=1,
 FIT='TIGHT',
 LEGEND = 'r = 0.6'
 XCOL = 1, YCOL = 2
 $END
11.6   -.122
31.9  -.009
72.6  -.008
110.7  -.01
143.7  -.009
204.6  -.005
236.1  -.006
266.5  -.001
END CURVE
 $OPTIONS
 LINE = 'SYMBOLS',SYMBOL=2,
 FIT='TIGHT',
 LEGEND = 'r = 0.7'
 XCOL = 1, YCOL = 2
 $END
11.6   -.261
31.9  -.080
72.6  -.015
110.7  -.015
143.7  -.008
204.6  -.01
236.1  -.016
266.5  -.009
END CURVE
 $OPTIONS
 LINE = 'SYMBOLS',SYMBOL=5,
 FIT='TIGHT',
 LEGEND = 'r = 0.8'
 XCOL = 1, YCOL = 2
 $END
11.6   -.568
31.9  -.263
72.6  -.061
110.7  -.030
143.7  -.010
204.6  -.017
236.1  -.018
266.5  -.007
END CURVE
 $OPTIONS
 LINE = 'SYMBOLS',SYMBOL=6,
 FIT='TIGHT',
 LEGEND = 'r = 0.9'
 XCOL = 1, YCOL = 2
 $END
11.6   -1.393
31.9  -.963
72.6  -.409
110.7  -.304
143.7  -.148
204.6  -.080
236.1  -.054
266.5  -.0430