Light metal alloys, as aluminium- and titanium based alloys, are of gr
eat interest to aerospace industry but thermodynamic information, main
ly heat capacity, is often missing. Then we measured on heating the he
at content of seven industrial titanium alloys from room temperature t
o 600-degrees-C with the help of a high-temperature Calvet calorimeter
(drop method). Their heat capacities were deduced by derivation of th
e enthalpy with respect to temperature. The departures from Kopp-Neuma
n law were calculated.