International Journal of Aerospace Engineering / 2018 / Article / Tab 10

Research Article

Aircraft Gas Turbine Engine Health Monitoring System by Real Flight Data

Table 10

ANOVA results for EGT training.

ANOVAa
ModelSum of squaresdfMean squareFSig.

1
 Regression12753394.9081594174.3631939.4320.000b
 Residual818692.113996821.980
 Total13572087.021004

aDependent variable: exhaust gas temperature. bPredictors: (constant), ground/air, vertical acceleration, pitch, roll, angle of attack, total air temperature, N2 speed, and N1 speed.