BERYLLIDE COMPOSITION 1 2400-DEGREE TURBINE/MATERIALS RESEARCH PROGRAM.
Abstract
The report summarizes the results of tests conducted on beryllide Composition 1 specimens during performance of the 2400-degree turbine/materials research program. The information contained herein is intended for presentation to U. S. Army Aviation Materiel Laboratories to show compliance with Contract DA44-177-AMC-183(T). The tests conducted include tensile, impact, stress-rupture, creep, thermal fatigue, oxidation, oxidation-sulfidation, and physical properties tests. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 17, 1967
- Accession Number
- AD0653632
Entities
People
- R. B. Scott