An approximate method of determining the subsonic flow in an arbitrary stream filament of revolution cut by arbitrary turbomachine blades

Chung-Hua Wu, Curtis A. Brown, Vasily D. Prian
naca-tn-2702
Jun 1952


A method is presented to obtain a relatively quick approximate determination of the detailed subsonic flow of a nonviscous fluid past arbitrary turbomachine blades. The governing equations are formulated as though the flow were constrained to stream filaments of revolution (the thicknesses of which vary as they pass through the machine).

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1952/naca-tn-2702.pdf