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

Table 4

Mass constraints.

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