It is a further aim of the present invention to provide a method for improving {HEAD ~ the fatigue life} of a thermally stressed portion of {TAIL ~ an aerodynamic surface} of a gas turbine engine 
It is a further aim of the present invention to provide a method for improving { HEAD ~ the fatigue life } of a thermally stressed portion of { TAIL ~ an aerodynamic surface } of a gas turbine engine
OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH HEAD HEAD HEAD HEAD HEAD HEAD HEAD OTH OTH OTH OTH OTH OTH TAIL TAIL TAIL TAIL TAIL TAIL TAIL OTH OTH OTH OTH OTH