Accession Number : ADA305093
Title : Fatigue Failure Analysis of Polycarbonate Transparencies in Different Environmental Conditions.
Descriptive Note : Final rept. 18 May 92-1 Oct 94,
Corporate Author : PURDUE RESEARCH FOUNDATION HAMMOND IN DEPT OF ENGINEERING
Personal Author(s) : Kin, Yulian B.
PDF Url : ADA305093
Report Date : DEC 1994
Pagination or Media Count : 54
Abstract : The investigation completed under the existing contract determines the extruded polycarbonate fatigue life dependency on elevated and cooling temperatures. The specimens were manufactured from the 1/2-inch flat polycarbonate sheet which is used as a structural component in laminates for some F-16 aircraft canopies. The results of the investigation showed that the elevated temperature is extremely dangerous. Fatigue lives of the specimens tested on different combinations of load and elevated temperature levels were always significantly (up to 10 times) less compared to those tested under the same load levels at room temperature. The surface topography failure modes also were different: ductile under room temperature and brittle under elevated temperatures. The investigations under cooling temperatures proved that the resistance to fatigue failure is substantially greater than that for room temperature.
Descriptors : *FATIGUE LIFE, *AIRCRAFT CANOPIES, *POLYCARBONATES, HIGH TEMPERATURE, LAMINATES, TOPOGRAPHY, ROOM TEMPERATURE, THERMAL ANALYSIS, FAILURE(MECHANICS), STRUCTURAL COMPONENTS, TRANSPARENCIES.
Subject Categories : Aircraft
Distribution Statement : APPROVED FOR PUBLIC RELEASE