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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2018
/
Article
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Tab 4
Research Article
Aircraft Gas Turbine Engine Health Monitoring System by Real Flight Data
Table 4
Validation data range used in the prediction of EGT.
Statistics
N1 speed
N2 speed
Pitch
Angle of attack
Roll
Vertical acceleration
Total air temperature
Ground/air
Exhaust gas temperature
N
Valid
215
215
215
215
215
215
215
215
215
Missing
0
0
0
0
0
0
0
0
0
Mean
59.6409302
80.8041860
1.791628
0.672093
−1.298140
1.000530
−4.323721
0.86
575.411628
Median
65.9000000
83.9000000
1.100000
−.400000
−1.400000
0.997000
−8.300000
1.00
572.000000
Std. deviation
25.67176527
10.77929528
3.6772253
1.7983021
4.4961766
0.0397756
17.7368312
0.347
108.3661869
Range
75.30000
37.80000
22.5000
7.1000
51.0000
0.4170
64.0000
1
421.5000
Minimum
20.60000
59.30000
−2.8000
−1.1000
−21.8000
0.8360
−24.0000
0
442.0000
Maximum
95.90000
97.10000
19.7000
6.0000
29.2000
1.2530
40.0000
1
863.5000