Thermo-Mechanical Behavior of 410 Stainless Steel Over a Wide Range of Strain Rates, Temperatures, and Loading Conditions

Details

• Creators:
  Ho, Chong-Wei
• Corporate Creators:
  Ohio State University. Dynamic Mechanics of Materials Laboratory (DMML)
• Corporate Contributors:
  United States. Federal Aviation Administration. Aircraft Certification Service Policy and Innovation Division
• Subject/TRT Terms:
  • Stainless steel
  • Plasticity
  • Flow
  • Strain measurement
  • Temperature
  • Digital simulation
  • Infrared detectors
  • Taylor-Quinney
  • Johnson-Cook
  • Hopkinson bar
• Publication/ Report Number:
  DOT/FAA/TCTT-26/29
• DOI:
  https://doi.org/10.21949/m49s-ta70
• Resource Type:
  Tech Report
• Geographical Coverage:
  United States
• Edition:
  Final Report
• Contracting Officer:
  Cordasco, Daniel
• Corporate Publisher:
  United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
• Abstract:
  This research investigates the thermomechanical behavior of 410 stainless steel under tension, compression, and torsion across a wide strain rate range from 10-4 s-1 to 5000 s-1. The material reveals identical yielding stresses across all loading modes, however, the material exhibits more pronounced hardening under tensile loading, followed by compression, with minimal hardening observed under torsion. The compressive loading analysis accounted for physical barreling by utilizing analytical methods and reverse engineering to correct the flow stress for frictional effects. Anisotropy testing shows Lankford coefficients close to 1.0 in tension.
• Format:
  PDF
• Funding:
  692M152340003
• Download URL:
  https://rosap.ntl.bts.gov/view/dot/93067/dot_93067_DS1.pdf
• File Type:
  [PDF - 9.26 MB]
• Collection(s):
  FAA William J. Hughes Technical Center for Advanced Aerospace
• Main Document Checksum:
  urn:sha-512:1d7f883d5969601968d58d9cf1a66c52d817c42c0a0417dbdda99d995af8a4c4fc4b943cf48dace46795200daaa79120c1dcf35f157f40b70247c27049a0e097