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Computed And Measured Flow In A Turnaround DuctReport presents theoretical and experimental study of subsonic flow of air in 180 degree-turnaround duct of rectangular cross section. Purpose of study to conduct partial simulation of conditions similar to those in axisymmetric duct of Space Shuttle main engine. Part of continuing effort to develop capability to simulate complicated turbulent internal flows with large curvatures like those in rocket engines and turbomachinery.
Document ID
19920000181
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Monson, Daryl J. (NASA Ames Research Center, Moffett Field, CA.)
Seegmiller, H. Lee (NASA Ames Research Center, Moffett Field, CA.)
Mcconnaughey, Paul K. (Marshall Space Flight Center)
Date Acquired
August 15, 2013
Publication Date
March 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-12614
Report Number: ARC-12614
ISSN: 0145-319X
Accession Number
92B10181
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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