NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Experimental investigation in an annular cascade sector of highly loaded turbine stator blading. 5 - Performance of two tangential jet bladesTesting low reaction jet turbine stator blades in six-blade annular cascade
Document ID
19710002752
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bettner, J. L. (General Motors Corp. Indianapolis, IN, United States)
Date Acquired
August 6, 2013
Publication Date
November 1, 1970
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
EDR-5315
NASA-CR-1675
Report Number: EDR-5315
Report Number: NASA-CR-1675
Accession Number
71N12227
Funding Number(s)
CONTRACT_GRANT: NAS3-9404
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available