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Pressure-distribution Measurements on the Rotating Blades of a Single-stage Axial-flow Compressor
Jack F. Runckel
Richard S. Davey
出版
National Advisory Committee for Aeronautics
, 1947
URL
http://books.google.com.hk/books?id=_WJDAQAAIAAJ&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
A preliminary investigation has been made of the pressure distribution about the mean-radius section of the rotating blades of a single-stage axial-flow compressor at a blade Mach number of 0.35. A 24-cell pressure-transfer device used in obtaining the pressure data is described and the accuracy of these data is established by several independent methods.
