DEVELOPMENT OF FATIGUE DATA FOR SEVERAL ALLOYS FOR USE IN AEROSPACE DESIGN.
Abstract
Manufacturing of all sheet specimens is 90% completed and the program is progressing into the testing stage. Tensile, fatigue, and stress rupture tests have begun. Fatigue of sheet specimens has been studied using an A ration of 0.5 (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 15, 1966
- Accession Number
- AD0804591
Entities
People
- F. C. Hagan