Thermal barrier coatings for gas turbine and diesel engines
By: Robert A. Miller, William J. Brindley, and M. Murray Bailey ; prepared for the Eleventh Workshop on Ceramic Coatings for Wear and Thermal Applications sponsored by the Canadian University-Industry-Council on Advanced Ceramics, Edmonton, Alberta, Canada, October 16-17, 1989.
Contributors: Brindley, W. J.; Bailey, M. Murray.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 102408.
Publisher: NASA; For sale by the National Technical Information Service
Published: 1990
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aircraft gas-turbines -- Materials -- Thermal properties.; Trucks -- Motors (Diesel) -- Materials -- Thermal properties.; Coatings -- Thermal properties.; Aerodynamic heating.; Ceramics.; Temperature effects.; Thermal control coatings.; Yttrium compounds.; Zirconium compounds.
Notes: Cover title.

Shipping list no.: 90-0561-M.

"Performing organization report no.: E-5160"--Technical rept. documentation p.

Includes bibliographical references (p. 5).

Also available via Internet from the NASA Technical Report Server web site. Address as of 5/19/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900004320%5F1990004320.pdf; current access available via PURL.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.

505-63-1A.