Determination of Selected MIL-HDBK-5 Design Allowable Properties for Five Aerospace Materials.
Abstract
This annual report describes a test program to develop certain missing MIL-HDBK-5 design allowable properties for five aerospace materials: 2024-T861 aluminum alloy sheet, 17-4PH and 15-5PH precipitation hardening stainless steel bar, 9Ni-4Co-0.20C steel plate, and Ti-6Al-6V-2Sn annealed extrusion. Design allowable properties were determined in accordance with MIL-HDBK-5 guidelines. Mechanical properties determined were Tensile yield strength; tensile ultimate strength; compressive yield strength; shear ultimate strength; bearing yield strength; bearing ultimate strength; compressive modulus of elasticity; Poisson's ratio; stress-strain curves; stress-tangent modulus curves, and high temperature properties.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1975
- Accession Number
- ADA013877
Entities
People
- Paul E. Ruff
Organizations
- Battelle Memorial Institute