Residual stresses in thermal barrier coatings for a Cu-8Cr-4Nb substrate system
By: Louis J. Ghosn, Sai V. Raj.
Contributors: Raj, Sai V.; NASA Glenn Research Center.
Series: NASA/TM -- 2002-211561.; NASA technical memorandum -- 211561.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for Aerospace Information
Published: 2002
Place of publication: [Cleveland, Ohio]; Hanover, MD
Language: eng
Format: Microform
Subjects: Finite element method.; Residual stress.; Rocket engines.; Surface roughness.; Plasma spraying.; Thermal stresses.; Coating.
Notes: Shipping list no.: 2003-0314-M.

"July 2002."

Also available via Internet from the Glenn Research Center Web site. Address as of 3/30/04: http://gltrs.grc.nasa.gov/reports/2002/TM-2002-211561.pdf; current access available via PURL.

Microfiche. [Washington, D.C.] : Supt. of Docs., U.S. G.P.O., [2003] 1 microfiche.