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

Table 4

Displacement response of the simulated engine system.

Position	Peak transient response (mm)	Amplitude of steady response (mm)
Low-pressure compressor disk	63.9	33.6
Low-pressure turbine disk	20.7	4.8
High-pressure compressor disk	10.4	2.3
High-pressure turbine disk	44.6	8.6