On Flight Risk Quantitative Evaluation under Icing Conditions

Table 6

Fitting test of extreme AOA.

Model	K-S		A-D		χ2
EV	0.2606	<0.0001	18.9411	<0.0001	15.5295
GEV	0.0516	0.6413	0.5574	0.6889	0.2089
Long	0.1427	0.0005	4.5021	0.0050	2.4380
Weibull	0.1711	<0.0001	9.8211	<0.0001	5.2385
Exp	0.4548	<0.0001	44.8035	<0.0001	18.1063
Norm	0.1941	<0.0001	10.3963	<0.0001	5.6621