The effect of O₂, H₂O, and N₂ on the fatigue crack growth behavior of an Ü + Ý titanium alloy at 24C̊ and 177C̊
By: Stephen W. Smith and Robert S. Piascik.
Contributors: Piascik, Robert S.; Langley Research Center.
Series: NASA/TM -- 2001-211248.; NASA technical memorandum -- 211248.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from NASA Center for AeroSpace Information (CASI)
Published: 2001
Place of publication: Hampton, Va; Hanover MD
Language: eng
Format: Microform
Subjects: Fatigue tests.; Fatigue (Materials); Crack propagation.; Titanium alloys.; Embrittlement.
Notes: Shipping list no.: 2003-0056-M.

Also available via Internet from the NASA web site. Address as of 2/24/03: http://techreports.larc.nasa.gov/ltrs/PDF/2001/tm/NASA-2001-tm211248.pdf ; current access is available via PURL.

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