Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material

An edition of Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material (2001)

Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material

By William M. Johnston

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Publish Date

2001

Publisher

National Aeronautics and Science Administration, Langley Research Center,Available from NASA Center for Aerospace Information

Language

eng

Pages

Description:

subjects: Aluminum alloys, Stress-strain relationships, Fracturing, Tensile tests, Static tests