Additively manufactured turbine shroud segment

A method of manufacturing a turbine shroud segment for a turbine shroud, comprising:

• thermally modeling, based on an expected thermal loading on the turbine shroud segment corresponding with an expected position of the turbine shroud segment within the turbine shroud, a first digital version of the turbine shroud segment to determine a first thermal model result of the first digital version, wherein the first digital version comprises a first parameter of a thermal management characteristic;
• thermally modeling, based on the expected thermal loading on the turbine shroud segment corresponding with the expected position of the turbine shroud segment within the turbine shroud, a second digital version of the turbine shroud segment to determine a second thermal model result of the second digital version, wherein the second digital version comprises a second parameter of the thermal management characteristic, and wherein the second parameter of the thermal management characteristic is different than the first parameter of the thermal management characteristic;
• selecting to manufacture the first digital version based on a comparison between the first thermal model result and the second thermal model result;
• and
• additively manufacturing the turbine shroud segment based on the first digital version.