An experimental investigation of the blade vibratory stresses in a single-stage compressor
The effect of Reynolds number on the performance of a single stage compressor
Blade vibratory stresses in a multi-stage axial flow compressor
The design and testing of an axial compressor having a mean stage temperature rise of 30 deg C
The design and testing of an axial flow compressor having different blade profiles in each stage
The design and testing of an axial flow compressor having different blade profiles in each stage