Turbine Engine Hot Section Technology (HOST).
- Oct 1, 1982.
- Physical Description:
- 1 electronic document
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- 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.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19850002643., Accession ID: 85N10951., NAS 1.15:83022., E-1458., NASA-TM-83022., and 19-20 Oct. 1982; Cleveland, OH; United States.
- No Copyright.
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