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NASA NTRS ยท 19720011124

Computer program for preliminary design analysis of axial-flow turbines

Abstract

The program method is based on a mean-diameter flow analysis. Input design requirements include power or pressure ratio, flow, temperature, pressure, and speed. Turbine designs are generated for any specified number of stages and for any of three types of velocity diagrams (symmetrical, zero exit swirl, or impulse). Exit turning vanes can be included in the design. Program output includes inlet and exit annulus dimensions, exit temperature and pressure, total and static efficiencies, blading angles, and last-stage critical velocity ratios. The report presents the analysis method, a description of input and output with sample cases, and the program listing.

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BibTeXRIS

Glassman, A. J.. 1972-03-01. Computer program for preliminary design analysis of axial-flow turbines. https://ntrs.nasa.gov/citations/19720011124

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