NASA NTRS · 19740012328
Hightip-speed, low-loading transonic fan stage. Part 2: Data compilation
Abstract
Tests were conducted on a high-tip-speed low-loading transonic fan stage to determine the performance and inlet flow distortion tolerance of the design. Test data were recorded for overall and blade element performance with both uniform and distorted inlet flows. A tabular summary of the data and a representative selection of the computer data reduction sheets are presented.
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Ware, T. C., Kobayashi, R. J., Jackson, R. J.. 1974-02-01. Hightip-speed, low-loading transonic fan stage. Part 2: Data compilation. https://ntrs.nasa.gov/citations/19740012328
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