Research Article
Minimization of Ground Vibration Test Configurations for F-16 Aircraft by Subtractive Modification
| # | 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 |
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