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

Figure 10

Verification of first five elastic modes (left: reference [16]; right: updated model): (a) mode 1-reference [11], (b) mode 1-updated model, (c) mode 2-reference [11], (d) mode 2-updated model, (e) mode 3-reference [11], (f) mode 3-updated model, (g) mode 4-reference [11], (h) mode 4-updated model, (i) mode 5-reference [11], and (j) mode 5-updated model.

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