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Propeller Design ProgramPlanform 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.
Document ID
19840000371
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Phillips, W. H.
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 4
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LAR-13142
LAR-13141
ISSN: 0145-319X
Report Number: LAR-13142
Report Number: LAR-13141
Accession Number
84B10371
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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