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Discharge Coefficients for Combustor-liner Air-entry Holes II : Flush Rectangular Holes, Step Louvers, and ScoopsExperimental discharge coefficients for various types of combustor-liner air-entry holes are presented as a function of a dimensionless flow parameter. In general, scoops and step louvers have higher discharge coefficients and wider flow ranges than flush holes. The effects of size or shape of a given type of hole are small. The proximity of multiple flush holes or the wall inclination of a convergent duct has a negligible effect on discharge coefficient.
Document ID
19930084900
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Dittrich, Ralph T
Date Acquired
August 16, 2013
Publication Date
April 1, 1958
Report/Patent Number
NACA-TN-3924
Accession Number
93R14190
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLOW, COMPRESSIBLE
COMBUSTION AND COMBUSTORS
FLOW, SUBSONIC
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