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The boundary layer on compressor cascade bladesSome redesign of the cascade facility was necessary in order to incoporate the requirements of the LDA system into the design. Of particular importance was the intended use of a combination of suction upstream of the blade pack with diverging pack walls, as opposed to blade pack suction alone, for spanwise dimensionality control. An ARL blade was used to redo some tests using this arrangement. Preliminary testing and boundary layer measurements began on the double circular arc blades.
Document ID
19820008172
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Deutsch, S.
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1981
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-165079
Report Number: NASA-CR-165079
Accession Number
82N16045
Funding Number(s)
CONTRACT_GRANT: NSG-3264
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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