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Experimental investigation in an annular cascade sector of highly loaded turbine stator blading. Volume 1 - Analysis and designApplication of boundary layer control concepts to highly loaded turbine stator blades in annular cascades
Document ID
19690004879
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bettner, J. L. (General Motors Corp. Indianapolis, IN, United States)
Date Acquired
August 5, 2013
Publication Date
December 1, 1968
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-1219
Report Number: NASA-CR-1219
Accession Number
69N14211
Funding Number(s)
CONTRACT_GRANT: NAS3-9404
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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