Approximate design method for high-solidity blade elements in compressors and turbines

John D. Stanitz
naca-tn-2408
Jul 1951


An approximate blade-element design method is developed for compressible or incompressible nonviscous flow in high-solidity stators or rotors of axial-, radial-, or mixed-flow compressors, turbines, or two-dimensional cascades.

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http://naca.central.cranfield.ac.uk/reports/1951/naca-tn-2408.pdf