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The influence of primary and secondary orientations on the elastic response of a nickel-base single-crystal superalloyThe influence of primary orientation on the elastic response of a (001)-oriented nickel-base single-crystal superalloy, PWA 1480, was investigated under mechanical, thermal, and combined thermal and mechanical loading conditions using finite element techniques. Elastic stress analyses were performed using the MARC finite element code on a square plate of PWA 1480 material. Primary orientation of the single crystal superalloy was varied in increments of 2 deg, from 0 to 10 deg, from the (001) direction. Two secondary orientations (0 and 45 deg) were considered, with respect to the global coordinate system, as the primary orientation angle was varied. The stresses developed within the single crystal plate were determined for each loading condition. In this paper, the influence of the angular offset between the primary crystal orientation and the loading direction on the elastic stress response of the PWA 1480 plate is presented for different loading conditions. The influence of primary orientation angle, when constrained between the bounds considered, was not found to be as significant as the influence of the secondary orientation angle, which is not typically controlled.
Document ID
19930017361
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Abdul-Aziz, Ali
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Kalluri, Sreeramesh
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Mcgaw, Michael A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1993
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-106125
NAS 1.15:106125
E-7801
Report Number: NASA-TM-106125
Report Number: NAS 1.15:106125
Report Number: E-7801
Meeting Information
Meeting: ASME International Gas Turbine and Aeroengine Congress and Exposition
Location: Cincinnati, OH
Country: United States
Start Date: May 24, 1993
End Date: May 27, 1993
Sponsors: ASME
Accession Number
93N26550
Funding Number(s)
PROJECT: RTOP 553-13-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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