A summary of experimental data is presented for a series of fracture tests and tensile tests that were conducted on a 2324-T39 aluminum alloy material. Static tensile tests were performed to determine the stress-strain response for the material. For the fracture tests three thicknesses (B = 0.5, 0.7, and 0.9-inches) and two specimen types (middle crack tension and compact tension specimens) were used. The middle crack tension specimens were 12-inches wide, and the compact tension specimens were 2, 4, and 6-inches wide. The fracture tests were conducted in the L-T orientation (crack perpendicular to the rolling direction and load parallel to the rolling direction).Johnston, William M. and Newman, James C., Jr. (Technical Monitor)Langley Research CenterFRACTURING; ALUMINUM ALLOYS; TENSILE TESTS; STRESS-STRAIN RELATIONSHIPS; STATIC TESTS; CRACKS; LOADS (FORCES); FRACTURE STRENGTH...