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NASA HOST Project OverviewNASA's Hot Section Technology (HOST) program has developed improved analytical models for the aerothermal environment, thermomechanical loading, material behavior, structural response, and service life of aircraft gas turbine engines' hot section components. These models, in conjunction with sophisticated computer codes, can be used in design analyses of critical combustor and turbine elements. Toward these ends, efforts were undertaken in instrumentation, combustion, turbine heat transfer, structural analysis, fatigue-fracture, and surface protection. Attention is presently given to the organization of HOST activities and their specific subject matter.
Document ID
19890010765
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
D E Sokolowski (Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1989
Publication Information
Publication: Toward Improved Durability in Advanced Aircraft Engine Hot Sections
Publisher: National Aeronautics and Space Administration
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: 33rd ASME International Gas Turbine and Aeroengine Congress and Exposition (IGTI)
Location: Amsterdam
Country: NL
Start Date: June 5, 1988
End Date: June 9, 1988
Sponsors: American Society of Mechanical Engineers
Accession Number
89N20136
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19890010764Collected WorksToward Improved Durability in Advanced Aircraft Engine Hot Sections
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