A combustor liner model for producing test data representative of a gas turbine engine combustor, said model comprising a plurality of members coupled together, said members comprising at least a first panel member and a second panel member, said first panel member fabricated from at least one of a pre-formed metallic cylinder section and a pre-formed metallic conical section, and comprising an inner surface and an outer surface, said second panel member fabricated from at least one of a pre-formed metallic conical section and a pre-formed metallic cylindrical portion, and comprising an inner surface and an outer surface, said first panel member coupled to said second panel member such that said first panel member and second panel member inner surfaces simulate an inner surface of the modeled gas turbine engine combustor, said model further comprising a plurality of templates coupled to at least one of said first and second panel member surfaces, said templates configured to contour at least one of said first and second panel member inner surfaces.