Browsing Aeronautical Research Council (1945-1979) by Author "C. E. Moss"

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The effect of inlet circumferential maldistribution on an axial compressor stage

R. C. Turner; J. Ritchie; C. E. Moss (1957)

This report describes tests on a single compressor stage with circumferentially non-uniform inlet conditions. The stage was a model of the first stage of a typical modern aircraft-engine compressor, and the tests were ...
The effect of reynolds number on the performance of a single-stage compressor

A. D. S. Carter; C. E. Moss; G. R. Green; G. G. Annear (1957)

In a preliminary report a description has been given of some tests on the effect of Reynolds number on the static-pressure rise through a single-stage axial-flow compressor. The work has since been extended and the full ...

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