NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Thermal Barrier CoatingsThermal barrier coatings offer gas turbines one way to reach fuel flexibility and improved efficiency. Test/analytical results are encouraging for this young technology.
Document ID
19780016348
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Grisaffe, S. J. (NASA Lewis Research Center Cleveland, OH, United States)
Levine, S. R. (NASA Lewis Research Center Cleveland, OH, United States)
Clark, J. S. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-78848
Report Number: NASA-TM-78848
Meeting Information
Meeting: Ann. Intern. Gas Turbine Conf.
Location: London
Start Date: April 9, 1978
End Date: April 13, 1978
Sponsors: ASME
Accession Number
78N24291
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available