Aircraft Gas Turbine Engine Health Monitoring System by Real Flight Data

Table 8

Model summary.

	Model summary^b
Model	R	R square	Adjusted R square	Std. error of the estimate	Change statistics
					R square change	F change	df1	df2	Sig. F change
1	0.969^a	0.940	0.939	28.6701942	0.940	1939.432	8	996	0.000

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