Transient Response of a Simulated Aeroengine with a Fusing Structure during a Fan-Blade Out Event

Table 8

Response of a low-pressure compressor disk with rub impact.

Position	Peak transient response (mm)	Amplitude of steady response (mm)
Rub impact	74.3	31.4
No rub impact	80.5	29.4
Relative deviation	7.7%	−6.8%