Impact Testing of Aluminum 2024 and Titanium 6Al-4V for Material Model Development

By: Administration (Nasa), National Aeronaut

One of the difficulties with developing and verifying accurate impact models is that parameters such as high strain rate material properties, failure modes, static properties, and impact test measurements are often obtained from a variety of different sources using different materials, with little control over consistency among the different sources. In addition there is often a lack of quantitative measurements in impact tests to which the models can be compared. To alleviate some of these problems, a project is underway to develop a consistent set of material property, impact test data and failure analysis for a variety of 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 FAA William J. Hughes Technical Center. Unique features of this set of data are that all material property data and impact test data are obtained using identical material, the test methods and procedures are extensively documented and all of the raw data is available. Four parallel efforts are currently underway: Measurement of material deformation and failure response over a wide range of strain rates and temperatures and failure analysis of material property specimens and impact test articles conducted by The Ohio State University; development of improved numerical modeling techniques for deformation and failure conducted by The George Washington University; impact testing of flat panels and substructures conducted by NASA Glenn Research Center. This report describes impact testing which has been done on aluminum (Al) 2024 and titanium (Ti) 6Al-4vanadium (V) sheet and plate samples of different thicknesses and with 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. Pereira, J. Michael and Revilock, Duane M. and Lerch, Bradley A. and Ruggeri, Charles R. Glenn Research Center NASA/TM-2013-217869, DOT/FAA/TC-12/58, E-18662 WBS 432938.11.01.03.02.02.16

• Format: Paperback
• Language: English
• ISBN: B08GG2DHH2
• ISBN13: 9798676289089
• Release Date: January 1
• Publisher: Independently Published
• Length: 86 Pages
• Weight: 0.49 lbs.
• Dimensions: 0.2" x 8.5" x 11.0"