The effects of shot and laser peening on fatigue life and crack growth in 2024 aluminum alloy and 4340 steel
By: R.A. Everett ... [et al.].
Contributors: Everett, R. A.; Langley Research Center.
Series: NASA/TM -- 2001-210843.; ARL-TR -- 2363.; NASA technical memorandum -- 210843.; ARL-TR (Aberdeen Proving Ground, Md.) -- 2363.
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: Aluminum alloys.; Crack propagation.; Fatigue life.; Steels.; Lasers.; Aircraft configurations.; Shot peening.
Notes: Shipping list no.: 2003-0056-M.

Also available via Internet from the NASA web site. Address as of 3/19/03: http://techreports.larc.nasa.gov/ltrs/PDF/2001/tm/NASA-2001-tm210843.pdf; current access is available via PURL.

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