Aeronautical Engineering/Axial fan design

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Question
I design axial fans using a method based on A J Stepanoff's work. While this has been successful, I think one aspect needs clarifying. He recommends solidity = 4.75 x head coefficient. I suspect a smaller constant than 4.75 is correct. If so, a slight improvement in efficiency could be realized by reducing skin drag.

Can you help?

Answer
Pat
I am not familiar with Stepanoff's work.  I would use the axial fan design methodology described by W. Rae and A. Pope:  Low-Speed Wind Tunnel Testing (2nd edition, John Wiley & Sons).  They include many parameters to arrive at solidity in the analysis and correlate efficiency with advance ratio and L/D. You could try your ideas in their procedure to see if you are moving in the right direction.
Paul

Aeronautical Engineering

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Paul Soderman

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Aeronautics, Fluid Mechanics, Aeroacoustics, Noise Control, Muffler Design, Wind Tunnel Research.... I know nothing about India - do not ask about schools, jobs, application requirements, career choices, etc. for India. Please, no text message verbiage; I prefer full words in full sentences. Thanks.

Experience

38 years as research engineer at NASA

Publications
AIAA, NASA

Education/Credentials
B.S. and M.S. Aeronautical Engineering - U. of Washington Graduate work Standford U.

Awards and Honors
AIAA Associate Fellow (American Institute of Aeronautics and Astronautics)

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