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FORTRAN program for computing coordinates of circular-arc, single and tandem, turbine and compressor, blade sections on a planeCoordinates for circular arc blade section of aircraft high speed compressor gas turbines were computed using FORTRAN 4 program. Aerodynamic configurations studied include single segment airfoils, airfoils with slots, and mutiple segment tandem arranged airfoil.
Document ID
19720000404
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mcnally, W. D.
Crouse, J. E.
Date Acquired
August 6, 2013
Publication Date
December 1, 1972
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LEW-11237
Report Number: LEW-11237
Accession Number
72B10405
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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