Verification and Baseline Fatigue Crack Growth Data of Ti-6-4, 430-195ksi Steel, and 7075-T73

Abstract

This research included baseline crack growth data for Ti-6-4 and 4340-195ksi steel, verification testing of the Ti-6-4 data, testing various geometries, and AFGROW development Baseline test data were produced for Ti-6-4 and 4340-195ksi. Center crack specimens were tested at four stress ratios. Load shedding enabled crack growth rates as low as 10.0(exp -9) to be recorded for both materials. Determining crack growth rates at this level is important for life predictions, since much of the life is accounted for when cracks are small. Open hole Ti-6-4 specimens were tested to verify the crack growth rate data generated and to test AFGROW's predictive abilities. For the six open hole specimens, AFGROW had an average error of 12%. Joint specimen also tested in order to verify AFGROW's abilities. These specimens were modeled with finite element analysis to determine the load transfer around the rivet holes. Once this was accomplished, predictions were run and compared to test data. The results of the single, multiple in-line joint, and multiple staggered joint specimens were good.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1997
Accession Number
ADA337794

Entities

People

  • J. A. Harter
  • J. H. Elsner
  • K. L. Boyd
  • S. Krishnan

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Amplitude
  • Bolted Joints
  • Bolts
  • Composite Materials
  • Diameters
  • Elements
  • Fasteners
  • Finite Element Analysis
  • Geometry
  • Materials
  • Stresses
  • Structural Integrity
  • Test Facilities
  • Two Dimensional
  • Verification

Fields of Study

  • Materials science

Readers

  • Computational Modeling and Simulation
  • Mechanical Engineering/Mechanics of Materials.
  • Psychological Intervention/Treatment for Stress, Anxiety, PTSD, and Related Emotional and Cognitive Health Symptoms.