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Computer program for preliminary design analysis of axial-flow turbinesThe 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.
Document ID
19720011124
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Glassman, A. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
E-6603
NASA-TN-D-6702
Report Number: E-6603
Report Number: NASA-TN-D-6702
Accession Number
72N18774
Funding Number(s)
PROJECT: RTOP 764-74
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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