Studies on Deformation and Failure Behavior of Ti-6Al-4V Alloy for Aircraft Structures
The IUP Journal of Mechanical Engineering, Vol. II, No. 3, pp. 58-70, August 2009
Posted: 13 Aug 2009
Date Written: August 13, 2009
Abstract
The dynamic response of Ti-6Al-4V alloy at high strain rate is investigated with tensile split Hopkinson bar test using plate type of specimens. High strain rate tensile tests are then performed with the above said material in order to construct their appropriate constitutive models for use in aircraft structures under dynamic conditions.
Keywords: Stress, Strain, Strain rate, Mechanical behavior
Suggested Citation: Suggested Citation
Ranjit, P. S. and Reddy, A. Chennakesava, Studies on Deformation and Failure Behavior of Ti-6Al-4V Alloy for Aircraft Structures (August 13, 2009). The IUP Journal of Mechanical Engineering, Vol. II, No. 3, pp. 58-70, August 2009, Available at SSRN: https://ssrn.com/abstract=1448383
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