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