columbus · Fracture Toughness, Fatigue and Corrosion Characteristics of X7080-T7E41 and 7178-T651 Plate and 7075-T6510, 7075-T73510, X7080-T7E42, and 7178-T6510 Extruded Shapes.

Fracture Toughness, Fatigue and Corrosion Characteristics of X7080-T7E41 and 7178-T651 Plate and 7075-T6510, 7075-T73510, X7080-T7E42, and 7178-T6510 Extruded Shapes.

Title: Fracture Toughness, Fatigue and Corrosion Characteristics of X7080-T7E41 and 7178-T651 Plate and 7075-T6510, 7075-T73510, X7080-T7E42, and 7178-T6510 Extruded Shapes.
Date: 1969
Index Abstract: Coming Soon
Photo Quality: Complete
Report Number: AFML TR 69-255
Creator: Kaufman, J. G.; Nordmark, G. E.; Lifka, B. W.; Coursen, J. W.; Schilling, P. E.
Corporate Author: Aluminum Company of America
Laboratory: Air Force Materials Laboratory
Extent: 332
Identifier: AD0864895
Access Rights: Export Controls
Distribution Classification: 1
Contract: F33615-67-C-1521
DoD Project: 7381
DoD Task: 738106
DTIC Record Exists: Yes
Distribution Change Authority Correspondence: AFSC USAF LTR
Distribution Conflict: No
Abstract: The tensile properties, plane-strain fracture toughness, axial-stress fatigue properties and fatigue-crack propagation rates, and the resistance to exfoliation and stress-corrosion cracking, were determined for several aluminum alloys. Two thicknesses of X7080-T7E41(T751) and 7178-T651 plate, and two thicknesses of 7075-T6510, 7075-T73510, X7080-T7E42(T7510) and 7178-T6510 extruded shapes, were evaluated.
Report Availability: Full text available
Date Issued: 1969-11
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Format: 1 online resource