Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material
By: William M. Johnston ; prepared ... under contract NAS1-96014.
Contributors: Langley Research Center.
Series: [NASA contractor report] -- NASA/CR-2001-210833.; NASA contractor report -- NASA CR-210833.
Publisher: National Aeronautics and Science Administration, Langley Research Center; Available from NASA Center for Aerospace Information
Published: 2001
Place of publication: Hampton, Va; Hanover, MD
Language: eng
Format: Microform
Subjects: Fracturing.; Aluminum alloys.; Tensile tests.; Stress-strain relationships.; Static tests.
Notes: Shipping list no.: 2002-0173-M.

"March 2001."

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