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Turbine Engine Hot Section Technology (HOST)Research and plans concerning aircraft gas turbine engine hot section durability problems were discussed. Under the topics of structural analysis, fatigue and fracture, surface protective coatings, combustion, turbine heat transfer, and instrumentation specific points addressed were the thermal and fluid environment around liners, blades, and vanes, material coatings, constitutive behavior, stress-strain response, and life prediction methods for the three components.
Document ID
19850002643
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Date Acquired
September 5, 2013
Publication Date
October 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:83022
NASA-TM-83022
E-1458
Accession Number
85N10951
Funding Number(s)
PROJECT: RTOP 533-04-1A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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