Hot salt stress corrosion tests have been performed on Ti 6246 smooth
test samples, under simulated gas turbine working conditions. The test
procedure has been optimised to be representative of these working co
nditions. The sample lifetime is measured and a mean crack velocity is
determined. A model based on surface self diffusion of the aggressive
species has been developed to describe the cracking. The influence of
the temperature on the model parameters is discussed. (C) 1998 Elsevi
er Science Ltd. All rights reserved.