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Analyses of Elemental Partitioning in Advanced Nickel-Base Superalloy Single CrystalsAircraft propulsion engines for the High Speed Civil Transport which may be developed early in the 21st century will require significantly different durability requirements than those which currently power civil aircraft. The durability will be more difficult to achieve because it is expected that the new aircraft engines will have to operate at near maximum power for more than half of each flight compared to 5 to 10 percent for typical current aircraft. To meet this requirement, a team of NASA, Pratt & Whitney Aircraft, and General Electric personnel have been formed to develop an appropriate alloy for the mission. This report summarizes the work performed by a part of that team up to the retirement of one of its members, R.L. Dreshfield. The prime purpose of the report is to assemble the data obtained in a single document so that it may be more accessible to those who may wish to pursue it at a later date.
Document ID
20050111501
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Dreshfield, Robert L.
(NASA Glenn Research Center Cleveland, OH, United States)
Thomas, Kimberly J.
(NYMA, Inc. Brook Park, OH, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
E-14735
NASA/TM-2005-213288
Report Number: E-14735
Report Number: NASA/TM-2005-213288
Funding Number(s)
WBS: WBS 22-714-09-46
Distribution Limits
Public
Copyright
Public Use Permitted.
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