Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application
By: Ali Abdul-Aziz, George Y. Baaklini, Ramakrishna T. Bhatt.
Contributors: Baaklini, George Y.; Bhatt, Ramakrishna T.; NASA Glenn Research Center.
Series: [NASA technical memorandum] -- NASA/TM-2001-210819.; NASA technical memorandum -- 210819.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for Aerospace Information
Published: 2001
Place of publication: [Cleveland, Ohio]; Hanover, MD
Language: eng
Format: Microform
Subjects: Silicon nitrides.; Finite element method.; Thermal stresses.; Thermal environments.; Hole geometry (Mechanics).; Air cooling.; Thermodynamic efficiency.; Ceramics.; Temperature distribution.; Stress analysis.; Ceramic coatings.
Notes: Shipping list no.: 2002-0336-M.

Also available via Internet from the NASA web site. Address as of 10/17/02: http://gltrs.grc.nasa.gov/reports/2001/TM-2001-210819.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002?] 1 microfiche.