NASA NTRS · 19840000371
Propeller Design Program
Abstract
Planform and propeller twist with minimum induced loss calculated. New Theoretical treatment combines classical theories of Betz-Prandtl, Goldstein, and Glauert easily applied to problem of determining propeller blade geometry for minimum induced loss. Analysis applicable at subsonic flight speeds and neglects structural considerations in propeller design.
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Phillips, W. H.. 1985-04-01. Propeller Design Program. https://ntrs.nasa.gov/citations/19840000371
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