Fatigue Failure Analysis of Polycarbonate Transparencies in Different Environmental Conditions.

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.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1994
Accession Number
ADA305093

Entities

People

  • Yulian B. Kin

Organizations

  • Purdue Research Foundation

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Canopies
  • Aircrafts
  • Contracts
  • Failure Analysis
  • Failure Mode And Effect Analysis
  • Fatigue Life
  • Laminates
  • Resistance
  • Structural Components
  • Topography
  • Transparencies

Fields of Study

  • Materials science

Readers

  • Materials Science (Mechanical Engineering).
  • Mechanical Engineering/Mechanics of Materials.