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Flow Through Gas-Turbine DuctsExisting computer program, Axisymmetric Diffuser Duct code (ADD code), modified to permit calculation of flows through small gas-turbine ducts with struts, guide vanes, and large degrees of turning. Code improvements include new coordinate generator, endwall loss model, and generalized geometry capability to describe struts and guide vanes in ducts that turn more than 90 degrees. Improved output format developed to provide solution on any arbitrary plane in duct.
Document ID
19850000533
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Anderson, O. L.
(United Technologies Corp.)
Hankins, G. B., Jr.
(United Technologies Corp.)
Edwards, D. E.
(United Technologies Corp.)
Date Acquired
August 12, 2013
Publication Date
March 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 9
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-14095
Report Number: LEW-14095
ISSN: 0145-319X
Accession Number
85B10533
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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