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Computer program for calculating aerodynamic forces on blade sectionsCalculation is taken from pressure or velocity distribution along blade surface. Blade sections have either one or two /tandem/ blade segments. Program is recommended primarily for use with ideal flow pressure distributions where forces in drag direction are neglected.
Document ID
19710000152
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mcnally, W. D.
Date Acquired
August 6, 2013
Publication Date
June 1, 1971
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LEW-11382
Report Number: LEW-11382
Accession Number
71B10153
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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