Research and Development Program to Develop a Nondestructive Evaluation Instrument (X-Ray Diffraction) for Measuring Residual Stresses in a Wide Range of Naval Aviation Material. Phase 2
Abstract
In the Phase II program a prototype stress analysis unit was designed, constructed, tested and delivered to the Navy that was smaller, lighter and easier to use than TEC's existing design. Also large number of residual stress measurements were made on components and materials of interest to Naval Aviation. Keywords: Residual stresses, X ray.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 03, 1987
- Accession Number
- ADA192507
Entities
People
- E. B. Pardue
- R. D. Brenner