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Views on the Impact of HOSTThe Hot Section Technology (HOST) Project, which was initiated by NASA Lewis Research Center in 1980 and concluded in 1987, was aimed at improving advanced aircraft engine hot section durability through better technical understanding and more accurate design analysis capability. The project was a multidisciplinary, multiorganizational, focused research effort that involved 21 organizations and 70 research and technology activities and generated approximately 250 research reports. No major hardware was developed. To evaluate whether HOST had a significant impact on the overall aircraft engine industry in the development of new engines, interviews were conducted with 41 participants in the project to obtain their views. The summarized results of these interviews are presented. Emphasis is placed on results relative to three-dimensional inelastic structural analysis, thermomechanical fatigue testing, constitutive modeling, combustor aerothermal modeling, turbine heat transfer, protective coatings, computer codes, improved engine design capability, reduced engine development costs, and the impacts on technology transfer and the industry-government partnership.
Document ID
19890010773
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
J B Esgar
(Sverdrup Maryland Heights, Missouri, United States)
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
89N20144
Distribution Limits
Public
Copyright
Public Use Permitted.
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