Two-dimensional flow on general surfaces of revolution in turbomachines

John D. Stanitz, Gaylord O. Ellis
naca-tn-2654
Mar 1952


A method of analysis is developed for two-dimensional flow on general surfaces of revolution in turbomachines with arbitrary blade shapes. The method of analysis is developed for steady, compressible, nonviscous, irrotational flow that is assumed uniform normal to the surfaces of revolution.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1952/naca-tn-2654.pdf