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Thermal/structural Tailoring of Engine Blades (T/SEAEBL). Theoretical 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 describes the T/STAEBL data block structure and system organization. The approximate analysis and optimization modules are detailed, and a validation test case is provided.
Document ID
19940024312
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)
Date Acquired
September 6, 2013
Publication Date
March 1, 1994
Subject Category
Structural Mechanics
Report/Patent Number
E-8495
NASA-CR-194462
NAS 1.26:194462
Accession Number
94N28815
Funding Number(s)
CONTRACT_GRANT: NAS3-22525
PROJECT: RTOP 505-63-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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