Minimization of Ground Vibration Test Configurations for F-16 Aircraft by Subtractive Modification

Table 7

Loading configurations.

#	Configuration 1	Configuration 2	Configuration 3	Configuration 4	Configuration 5
1	AA1	AA1	LAU-129	AA1	AA1
2	AA2	AA1	AA2	AA1	AA2
3	GBU31	GBU31	GBU31	GBU31	16S1700
4	Tank-1	Tank-1	Tank-1	Tank-1	Tank-1
5L	P-1	P-1	P-1	P-1	P-1
5	Tank-2	Tank-2	Tank-2	Tank-2	Tank-2
5R	P-2	P-2	P-2	P-2	P-2
6	Tank-1	Tank-1	Tank-1	Tank-1	Tank-1
7	GBU31	GBU31	GBU31	GBU31	GBU31
8	AA2	AA1	AA2	AA2	AA2
9	AA1	AA1	AA1	AA1	AA1