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Review and assessment of the database and numerical modeling for turbine heat transferThe objectives of the HOST Turbine Heat Transfer subproject were to obtain a better understanding of the physics of the aerothermodynamic phenomena and to assess and improve the analytical methods used to predict the flow and heat transfer in high-temperature gas turbines. At the time the HOST project was initiated, an across-the-board improvement in turbine design technology was needed. A building-block approach was utilized and the research ranged from the study of fundamental phenomena and modeling to experiments in simulated real engine environments. Experimental research accounted for approximately 75 percent of the funding while the analytical efforts were approximately 25 percent. A healthy government/industry/university partnership, with industry providing almost half of the research, was created to advance the turbine heat transfer design technology base.
Document ID
19880066914
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gladden, H. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Simoneau, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: Toward improved durability in advanced aircraft engine hot sections
Location: Amsterdam
Country: Netherlands
Start Date: June 5, 1988
End Date: June 9, 1988
Sponsors: ASME
Accession Number
88A54141
Distribution Limits
Public
Copyright
Other

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