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Edge geometry of turbomachine bladesComputer program calculates leading- and trailing-edge circle radii, tangency angles on leading- and trailing-edge circles, and stagger angle of turbomachinery blade sections, using only spline points defining blade surfaces.
Document ID
19780000262
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Schumann, L. F. (U. S. Army Air Mobility R and D Lab.)
Date Acquired
August 9, 2013
Publication Date
October 1, 1978
Publication Information
Publication: NASA Tech Briefs
Volume: 3
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-12979
Accession Number
78B10262
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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