Impact Testing of 410 Stainless Steel for Material Impact Model Development

Details

• Creators:
  Revilock, Duane M. ; Ruggeri, Charles R. ; Pereira, J. Michael
• Corporate Creators:
  Glenn Research Center ; United States. National Aeronautics and Space Administration
• Corporate Contributors:
  United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
• Subject/TRT Terms:
  Development Impact Tests Materials Tests Stainless Steel
• Publication/ Report Number:
  DOT/FAA/TC-25/22 ; NASA/TM-20260000491
• DOI:
  https://doi.org/10.21949/1prv-7323
• Resource Type:
  Tech Report
• Geographical Coverage:
  United States
• Edition:
  NASA STI Program Report Series
• Corporate Publisher:
  United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
• Abstract:
  A project is underway to develop a consistent set of material properties, impact test data, and failure analysis for a variety of metallic aircraft materials that can be used to develop improved impact failure and deformation models. This project is jointly funded by the NASA Glenn Research Center and the Federal Aviation Administration William J. Hughes Technical Center. Particular features of this set of data are that all material property and impact test data are obtained using traceable material, the test methods and procedures are extensively documented, and all the raw data are available. Four parallel efforts are currently underway: measurement of material deformation and failure response over a wide range of strain rates and temperatures, failure analysis of material property specimens and impact test articles, development of improved numerical modeling techniques for deformation and failure, and impact testing of flat panels and substructures for model validation.
  
  This report describes impact testing performed on 410 stainless steel sheet and plate samples of different thicknesses with two different types of projectiles, one a regular cylinder and one with a more complex geometry incorporating features representative of a jet engine fan blade. Data from this testing will be used in validating material models developed under this program. The material tests and the material models developed in this program will be published in separate reports.
  
  
• Format:
  PDF
• Collection(s):
  FAA William J. Hughes Technical Center for Advanced Aerospace
• Main Document Checksum:
  urn:sha-512:2299d21cfff5df8eaa0395f174d8311a795fc0e8d4fb6c78fa15d9de7c97976ea24f33bc52fb04f12706f91e7598ea5c0f90687c8b9b35fe72f00f366339c237
• Download URL:
  https://rosap.ntl.bts.gov/view/dot/90209/dot_90209_DS1.pdf
• File Type:
  [PDF - 47.88 MB ]