Research Article
Minimization of Ground Vibration Test Configurations for F-16 Aircraft by Subtractive Modification
Table 2
Configurations for model updating.
| | Station | Load |
| | 1 | LAU-129 + AIM-120 (AA1) | | 2 | 16S301 + 16S210 + AIM-9 (AA2) | | 3 | 16S1700 + GBU31 JDAM (GBU31) | | 4 | 370 gal empty fuel tank plus pylon (Tank-1) | | 5L | AAQ-13 (P-1) | | 5 | 300 gal empty fuel tank plus pylon (Tank-2) | | 5R | AAQ-14 (P-2) | | 6 | 370 gal empty fuel tank plus pylon (Tank-1) | | 7 | 16S1700 + GBU31 JDAM (GBU31) | | 8 | 16S301 + 16S210 + AIM-9 (AA2) | | 9 | LAU-129 + AIM-120 (AA1) |
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