Research Article
Minimization of Ground Vibration Test Configurations for F-16 Aircraft by Subtractive Modification
| Mass area | Target value (kg) |
| Stations 1–9 | 195 | Stations 2–8 | 130 | Stations 3–7 | 935 | Stations 4–6 | 200 | Station 5 | 240 | Wing | 1000 | Horizontal stabilizer | 170 | Vertical stabilizer | 180 | Fuselage | 7600 |
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