Accession Number : ADA301816
Title : Time-Temperature-Stress Capabilities of Composite Materials for Advanced Supersonic Technology Applications.
Descriptive Note : Monthly progress rept. no. 49, 1 Jul-1 Aug 77,
Corporate Author : GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV
Personal Author(s) : Haskins, J. F. ; Kerr, J. R.
PDF Url : ADA301816
Report Date : 01 AUG 1977
Pagination or Media Count : 8
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.
Descriptors : *STRESS ANALYSIS, *COMPOSITE MATERIALS, TEST AND EVALUATION, TEMPERATURE, TENSILE STRESS, STRENGTH(MECHANICS), LONG RANGE(TIME), TIME, RESIDUALS, BONDED JOINTS, SUPERSONIC FLIGHT, QUALITY ASSURANCE, FAILURE(MECHANICS), GRAPHITED MATERIALS, SUPERSONIC CHARACTERISTICS, FLIGHT SIMULATION, FATIGUE TESTS(MECHANICS), EXPOSURE METERS.
Subject Categories : Laminates and Composite Materials
Distribution Statement : APPROVED FOR PUBLIC RELEASE