An experimental investigation of the generation and consequences of acoustic waves in an axial flow compressor: Large axial spacings between blade rows
Review articleOpen access

AbstractThe excitation of acoustic modes in the annulus of a single stage, low speed, axial flow compressor was investigated experimentally. The modes were excited by vortex shedding from the inlet guide vanes and each mode was found to be associated with a number of rotor blade vibration excitation frequencies.

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