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T/BEST: Technology Benefit Estimator Select Features and ApplicationsA Technology Benefit Estimator (T/BEST) system has been developed to provide a formal method to assess advanced aerospace technologies and quantify the benefit contributions for prioritization. An open-ended, modular approach is used to allow for upgrade and insertion of advanced technology modules. T/BEST's software framework, beginner-to-expert operation, interface architecture, and key analysis modules are discussed. In this paper, selected features and applications of T/BEST are demonstrated. Sample cases pertaining to structural analysis of titanium and composite blades are presented. The performance of hot and cold composite fan blades is also discussed. The cost required to manufacture titanium and composite fan blades is estimated.
Document ID
19960045701
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Generazio, Edward R.
(NASA Cleveland, OH United States)
Chamis, Christos C.
(NASA Cleveland, OH United States)
Abumeri, Galib H.
(NYMA, Inc. Brook Park, OH United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1995
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:106960
NASA-TM-106960
REPT-E-9714
Report Number: NAS 1.15:106960
Report Number: NASA-TM-106960
Report Number: REPT-E-9714
Meeting Information
Meeting: International Symposium and Exhibition
Location: Anaheim, CA
Country: United States
Start Date: May 8, 1995
End Date: May 11, 1995
Sponsors: Society for the Advancement of Materials and Process Engineering
Accession Number
96N32586
Funding Number(s)
CONTRACT_GRANT: NAS3-27186
PROJECT: RTOP 505-63-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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