This file contains the output points from the average analysis of a blade. These files can be "averaged" to produce the mean airfoil from a set of airfoils. This is particularly useful in engineering applications, including reverse engineering.
!******* Start of Example AVG File ******************
FLAVOR C:\BladeRunner\blades\1234\GE_NO_BESTFIT.flv
PART 1234_AVG
NOMINAL C:\BladeRunner\blades\1234\124E4074.nom
TOLERANCE C:\BladeRunner\blades\1234\1234.tol
RADIUS 0.0
TEXT AVG_METHOD=NOM
CALCS 8
TETHCK
MAXTHK
CHORD
TWIST
CCMIN
CCMAX
CVMIN
CVMAX
PLATFORM 0
NUM_SECT 3
SECT1 112
0.727373 -1.337636 1.875000
0.722358 -1.327370 1.875000
0.716484 -1.314291 1.875000
0.709277 -1.298257 1.875000
0.701149 -1.278499 1.875000
0.691115 -1.255131 1.875000
0.679481 -1.227347 1.875000
0.665838 -1.195288 1.875000
0.650235 -1.158923 1.875000
0.632765 -1.118459 1.875000
0.613132 -1.073876 1.875000
!******* End of Example AVG File ******************
For more information, see "Average a Set of Report Files".