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Thermal/structural Tailoring of Engine Blades (T/STAEBL) User's ManualThe Thermal/Structural Tailoring of Engine Blades (T/STAEBL) system is a family of computer programs executed by a control program. The T/STAEBL system performs design optimizations of cooled, hollow turbine blades and vanes. This manual contains an overview of the system, fundamentals of the data block structure, and detailed descriptions of the inputs required by the optimizer. Additionally, the thermal analysis input requirements are described as well as the inputs required to perform a finite element blade vibrations analysis.
Document ID
19940022189
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brown, K. W.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Clevenger, W. B.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Arel, J. D.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1994
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:194463
NASA-CR-194463
PWA-5774-119
E-8496
Report Number: NAS 1.26:194463
Report Number: NASA-CR-194463
Report Number: PWA-5774-119
Report Number: E-8496
Accession Number
94N26692
Funding Number(s)
PROJECT: RTOP 505-63-5B
CONTRACT_GRANT: NAS3-22525
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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