NASA NTRS · 19800005795
Modification of axial compressor streamline program for analysis of engine test data
Abstract
An existing axial compressor streamline analysis computer program to allow input of measured radial pressure and temperature profiles obtained from engine or cascade data is described. The proposed modifications increase the input flexibility and are accomplished without changing the computer program's input format.
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Williams, J. G.. 1979-11-01. Modification of axial compressor streamline program for analysis of engine test data. https://ntrs.nasa.gov/citations/19800005795
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