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Data On Flow About A Compressor Blade In CascadeDevelopment and testing of software to compute values of flow-field characteristics greatly enhanced by using recorded experimental data to test results of computations. Report "The Measurement Of Boundary Layers On Compressor Blade In Cascade" is data base providing detailed measurements of boundary layer and wake in flow field about double-circular-arc compressor blades in cascade of such blades.
Document ID
19930000785
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Deutsch, S. (Pennsylvania State Univ.)
Zierke, W. C. (Pennsylvania State Univ.)
Date Acquired
August 16, 2013
Publication Date
December 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 12
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-15272
Report Number: LEW-15272
ISSN: 0145-319X
Accession Number
93B10785
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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