NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Secondary flows and three-dimensional boundary-layer effectsSecondary and three-dimensional boundary layer flows in compressor blade rows
Document ID
19650013759
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hansen, A. G. (NASA Lewis Research Center Cleveland, OH, United States)
Herzig, H. Z. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Aerodynamics
Accession Number
65N23360
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BOUNDARY LAYER FLOW
THREE-DIMENSIONAL BOUNDARY LAYER
SECONDARY FLOW
COMPRESSOR BLADE
Document Inquiry

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19650013744Collected WorksAerodynamic Design of Axial-Flow Compressors
No Preview Available