Paper 22: Transient Flows in Short Curved Diffusers
The work reported is the first stage of an investigation into the effect of pressure waves of varying amplitude on the flow through the blade passages of turbomachines. Attention is confined to the interaction between the pressure wave and the geometry of four curved diffusers with the same area distribution about a circular- arc centre-line. The geometry of these diffusers is based on a straight diffuser with a total divergence angle equal to 12° and a length of 5 in. The nominal turning angles are 30°, 45°, 60°, and 90°. The transient flow through the five diffusers has been compared on the basis of sequences of Schlieren photographs taken at 50 μs intervals. The attenuation of the wave at the curved walls has also been measured. Systematic measurements have been made of the net and transmitted pressures, and also the pressures on the curved walls, during the quasi-steady régime. An attempt has been made to predict the net and transmitted pressures by means of two simple analyses, one of which is moderately successful. Diffuser effectiveness has been compared under conditions of steady and quasi-steady flow.