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

See all articles by P. S. Ranjit

P. S. Ranjit

University of Petroleum & Energy Studies (UPES)

A. Chennakesava Reddy

JNTU Ananthapur

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

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

P. S. Ranjit (Contact Author)

University of Petroleum & Energy Studies (UPES) ( email )

Energy Acres
P.O. Bidholi via Premnagar,
Dehradun, IN Uttarakhand 248007
India

A. Chennakesava Reddy

JNTU Ananthapur ( email )

Kukatpally
Andhra Pradesh
Kakinada, Andhra Pradesh
India

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