PSI - Issue 71

M. Mohan Kumar et al. / Procedia Structural Integrity 71 (2025) 333–339

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Strain Gauge

Strain Gauge

Strain Gauge

Fig. 8. Test and FEA strain results comparison in One Wheel Landing DLL case (up to 100% DLL).

(a) Deflection of LH and RH Wing at T.E

(b) Deflection of LH and RH Wing at L.E

Fig. 9. Variation of deflection v/s % Load at TE and LE (LHS & RHS) for One Wheel Landing case.