High temperature fatigue crack growth behavior of Alloy 10
By: John Gayda.
Contributors: NASA Glenn Research Center.
Series: [NASA technical memorandum] -- NASA/TM-2001-210814.; NASA technical memorandum -- 210814.
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: Crack propagation.; Engine design.; Fracture strength.; Heat of solution.; High strength alloys.; Niobium.; Tantalum.; Thermal fatigue.
Notes: Shipping list no.: 2003-0084-M.

Also available via Internet from the NASA web site. Address as of 2/14/03: http://gltrs.grc.nasa.gov/reports/2001/TM-2001-210814.pdf ; current access is available via PURL.

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