Time-Temperature-Stress Capabilities of Composite Materials for Advanced Supersonic Technology Applications.
Abstract
Two doubler bond failures have occurred in the unidirectional B/A1 flight simulation specimens. New doublers will be attached, and the specimens will be returned to test. The residual strength testing of the Phase I B/E and G/E flight simulation specimens and the specimen configurations are discussed. Quality assurance testing of the full size G/PI Phase II panel was completed and results are presented. In the screening test portion of the new material evaluation full size panels of HT-S/PMR-15 and HT-S/710 have been fabricated and submitted for quality assurance testing.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1977
- Accession Number
- ADA301816
Entities
People
- J. F. Haskins
- J. R. Kerr
Organizations
- General Dynamics