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SUMMARY:High strain rate deformation response of titanium for aerospace ga
 s turbines - Steven Lainé\, Department of Materials Science\, The Univers
 ity of Cambridge
DTSTART:20170504T150000Z
DTEND:20170504T160000Z
UID:TALK66399@talks.cam.ac.uk
CONTACT:Stephen Walley
DESCRIPTION:Titanium has been used extensively and successfully in the aer
 ospace industry since the 1950s. Nevertheless\, there is a noticeable lack
  of understanding of high strain rate deformation\, deformation twinning m
 odes and the microscale mechanics during the high strain rate deformation 
 of titanium alloys in ambient conditions. Using ballistic impact testing\,
  commercial purity titanium and Ti–6Al–4V were tested at room temperat
 ure\, at a strain rate of 10^3 s−1. The results have important implicati
 ons for aerospace titanium alloys in gas turbine engines\, in particular T
 i–6Al–4V alloys for fan blade and compressor blade applications.\n
LOCATION:Mott Seminar Room\, Cavendish Laboratory
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