Ballistic Impact Simulations of a Titanium 6Al-4 V Generic Fan Blade Fragment on an Aluminum 2024 Panel Using *MAT_224 in LS-DYNA
Publication: Earth and Space 2022
ABSTRACT
As a part of the FAA’s Aircraft Catastrophic Failure Prevention Program, advanced Aluminum 2024 and Titanium 6Al-4 V material models utilizing *MAT_224 in LS-DYNA have been developed to improve the numerical modeling of turbine engine blade-out containment tests required for certification of aircraft engines. In this effort, NASA conducted four ballistic impact tests on large flat Aluminum 2024 panels with a blade-shaped Titanium 6Al-4 V projectile to provide experimental data to evaluate the numerical material model. These tests were designed to represent a realistic turbine engine fan-blade release event. In this research, ballistic impact tests were simulated using advanced Aluminum 2024 and Titanium 6Al-4 V material models to validate the material models under simulated turbine engine blade release event conditions. The research also identifies possible challenges for such a ballistic impact simulation with a blade-shaped projectile that slides, bends (plastically deforms), may fracture, and rotates as it moves in three dimensions.
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REFERENCES
Buyuk, M. (2014). Development of a New Metal Material Model in LS-DYNA, Part 2: Development of a Tabulated Thermo-Viscoplastic Material Model with Regularized Failure for Dynamic Ductile Failure Prediction of Structures under Impact Loading. Final Report, DOT/FAA/TC-13/25 P2, Federal Aviation Administration, U.S. Department of Transportation.
Dong, H., & Bell, T. (1999). “Tribological Behaviour of Alumina Sliding against Ti6Al4V in Unlubricated Contact.” Wear, 874–884.
Emmerling, W., Altobelli, D., Carney, K., & Pereira, M. (2014). Development of a New Metal Material Model in LS-DYNA, Part 1: FAA, NASA, and Industry Collaboration Background. Technical Report, DOT/FAA/TC-13/25 P1, Federal Aviation Administration, U.S. Department of Transportation.
Haight, S., Wang, L., Du Bois, P., Carney, K., & Kan, C. D. (2016). Development of a Titanium Alloy Ti-6Al-4V Material Model Used in LS-DYNA. Final Report, DOT/FAA/TC-15/23, Federal Aviation Administration, U.S. Department of Transportation.
Hammer, J. T. (2014). Plastic Deformation and Ductile Fracture of Ti-6Al-4V under Various Loading Conditions. Technical Thesis, DOT/FAA/TC-TT14/2, Federal Aviation Administration, U.S. Department of Transportation.
Kelley, S., & Johnson, G. (2006). Statistical Testing of Aircraft Materials for Transport Airplane Rotor Burst Fragment Shielding. Final Report, DOT/FAA/AR-06/9, Federal Aviation Administration, U.S. Department of Transportation.
LS-DYNA Aerospace Working Group. (2021). Retrieved from https://awg.lstc.com/tiki-index.php?page=Material+Parameter+Sets
LSTC. (2017). LS-DYNA Keyword User’s Manual, Volumes I and II, Version R10.0. Livermore, California: Livermore Software Technology Corporation.
Mishra, A. (2014). “Analysis of Friction and Wear of Titanium Alloys.” International Journal of Mechanical Engineering and Robotics Research, 3(3), 570–573.
Park, C. K., Carney, K., Du Bois, P., Cordasco, D., & Kan, C. D. (2020). Aluminum 2024-T351 Input Parameters for *MAT_224 in LS-DYNA. Final Report, DOT/FAA/TC-19/41 P1, Federal Aviation Administration, U.S. Department of Transportation.
Park, C. K., Queitzsch, G., Carney, K., Du Bois, P., Kan, C. D., Cordasco, D., & Emmerling, W. (2020). Aluminum 2024-T351 Input Parameters for *MAT_224 in LS-DYNA, Part 3: Ballistic Impact Simulations of an Aluminum 2024 Panel Using *MAT_224 in LS-DYNA Considering Oblique Incidence and Attitude Angles of a Rectangular Projectile. Final Report, DOT/FAA/TC-19/41 P3, Federal Aviation Administration, U.S. Department of Transportation.
Park, C. K., Carney, K., Du Bois, P., Kan, C. D., & Cordasco, D. (2021). Aluminum 2024-T351 Input Parameters for *MAT_224 in LS-DYNA, Part 4: Ballistic Impact Simulations of a Titanium 6Al-4 V Generic Fan Blade Fragment on an Aluminum 2024 Panel Using *MAT_224 in LS-DYNA. Final Report, DOT/FAA/TC-19/41 P4, Federal Aviation Administration, U.S. Department of Transportation.
Pereira, M., Revilock, D., Lerch, B., & Ruggeri, C. (2013). Impact Testing of Aluminum 2024 and Titanium 6Al-4 V for Material Model Development. Technical Memorandum, NASA/TM–2013–217869, DOT/FAA/TC-12/58, National Aeronautics and Space Administration.
Seidt, J. D. (2014). Development of a New Metal Material Model in LS-DYNA, Part 3: Plastic Deformation and Ductile Fracture of 2024 Aluminum under Various Loading Conditions. Final Report, DOT/FAA/TC-13/25 P3, Federal Aviation Administration, U.S. Department of Transportation.
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Published online: Jan 5, 2023
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