Research Article
Minimization of Ground Vibration Test Configurations for F-16 Aircraft by Subtractive Modification
| | Load and location | Mass (kg) | CG from nose (m) | Length (m) | Yaw inertia (kgm2) | Pitch inertia (kgm2) |
| | LAU-129 (WTR&WTL) | 39.5 | — | 3.44 | 18.8 | 18.8 | | AIM-120 (A120R&A120L) | 156 | 2.1 | 2.37 | 131 | 131 | | 16S210 (ULR&ULL) | 31 | — | 2.62 | 15.8 | 15.8 | | 16S301 (ULR&ULL) | 9 | — | — | — | — | | AIM-9 (ULR&ULL) | 91 | 1.8 | 2.62 | 70 | 70 | | 16S1700 (MPR&MPL) | 161 | — | 1.54 | 19.4 | 18.3 | | GBU31 JDAM (MR&ML) | 934 | 1.59 | 3.65 | 553 | 553 | | 370 gal fuel tank (DR&DL) | 199 | 2.32 | 5.45 | 239 | 225 | | 300 gal fuel tank (CL) | 242 | 2.2 | 4.42 | 224 | 224 | | AAQ-13 | 204 | — | — | — | — | | AAQ-14 | 249 | — | — | — | — |
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