NASA NTRS · 19750003110
Secondary vorticity in axial compressor blade rows
Abstract
A theoretical investigation of secondary flow in compressor blade rows is presented. Formulas for calculating secondary flows in annular cascade blade passages are derived. The influence of the relative rotation vector on secondary velocity perturbations, using recent developments in shear-flow theory, is examined. A method of calculating the flow through successive blade rows is given and a comparison is made with experimental results.
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Dixon, S. L.. 1974-01-01. Secondary vorticity in axial compressor blade rows. https://ntrs.nasa.gov/citations/19750003110
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