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Burner liner thermal/structural load modeling: TRANCITS program user's manualTransfer Analysis Code to Interface Thermal/Structural Problems (TRANCITS) is discussed. The TRANCITS code satisfies all the objectives for transferring thermal data between heat transfer and structural models of combustor liners and it can be used as a generic thermal translator between heat transfer and stress models of any component, regardless of the geometry. The TRANCITS can accurately and efficiently convert the temperature distributions predicted by the heat transfer programs to those required by the stress codes. It can be used for both linear and nonlinear structural codes and can produce nodal temperatures, elemental centroid temperatures, or elemental Gauss point temperatures. The thermal output of both the MARC and SINDA heat transfer codes can be interfaced directly with TRANCITS, and it will automatically produce stress model codes formatted for NASTRAN and MARC. Any thermal program and structural program can be interfaced by using the neutral input and output forms supported by TRANCITS.
Document ID
19860015460
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Maffeo, R.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:174891
NASA-CR-174891
R85AEB452
Report Number: NAS 1.26:174891
Report Number: NASA-CR-174891
Report Number: R85AEB452
Accession Number
86N24931
Funding Number(s)
CONTRACT_GRANT: NAS3-23272
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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