TITANIUM (6 A1-4V), HEAT TREATMENT OF
Abstract
Phase I: The current heat treatment for 6 Al 4V was modified to obtain the maximum strength without beta embrittlement. Tensile tests were conducted to determine the increase in strength obtained. Phase II: This part of the investigation was cancelled in lieu of a literature search for other titanium alloys with greater heat treatment response and hardenability. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1958
- Accession Number
- AD0285376
Entities
People
- R.j. Mcclintick
Organizations
- General Dynamics