NASA NTRS · 19860003827
A FORTRAN computer code for calculating flows in multiple-blade-element cascades
Abstract
A solution technique has been developed for solving the multiple-blade-element, surface-of-revolution, blade-to-blade flow problem in turbomachinery. The calculation solves approximate flow equations which include the effects of compressibility, radius change, blade-row rotation, and variable stream sheet thickness. An integral equation solution (i.e., panel method) is used to solve the equations. A description of the computer code and computer code input is given in this report.
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Mcfarland, E. R.. 1985-11-01. A FORTRAN computer code for calculating flows in multiple-blade-element cascades. https://ntrs.nasa.gov/citations/19860003827
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