As result of the conditional averaging analysis there are 3 Tecplot-files for each flight case.
In all results defect sensors and interpolations are considered.

XXXX_YY_80.tec : Values of 80 successive rotor revolutions 
XXXX_YY_sa.tec : Simple averaged values of one revolution
XXXX_YY_ca.tec : Conditional averaged values of one revolution

XXXX : CnM2 = normal force coefficient * square of Mach number
       CmM2 = moment coefficient about c/4 * square of Mach number

YY :   BL = Dpt 128
       MN = Dpt 413
       MV = Dpt 485