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Pre-HOST high temperature crack propagationThe highlights of NASA contract CR-167896, Fracture Mechanics Criteria for Turbine Engine Hot Section Components, are presented. The five technical tasks of the program are reviewed. Results of several tasks are presented.
Document ID
19850002648
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Orange, T. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1982
Publication Information
Publication: Turbine Eng. Hot Sect. Technol. (HOST)
Subject Category
Aircraft Propulsion And Power
Accession Number
85N10956
Distribution Limits
Public
Copyright
Public Use Permitted.

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IDRelationTitle19850002643Collected WorksTurbine Engine Hot Section Technology (HOST)
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