A system, comprising: a gas turbine enclosure; a gas turbine engine disposed in the gas turbine enclosure; an air intake system operatively coupled to the gas turbine enclosure to direct air to the gas turbine engine, wherein the air intake system includes an air filter house to filter the air directed to the gas turbine engine; a gas turbine combustion exhaust operatively coupled to the gas turbine engine to output an exhaust flow generated from the gas turbine engine outside of the gas turbine enclosure; low pressure recoup air piping operatively coupled to the gas turbine engine, the gas turbine enclosure and the gas turbine combustion exhaust to provide low pressure recoup air vented from the gas turbine engine to the gas turbine combustion exhaust and/or the gas turbine enclosure; a first valve operatively coupled to the low pressure recoup air piping to control a flow of the low pressure recoup air to the gas turbine combustion exhaust; a second valve operatively coupled to the low pressure recoup air piping for diverting the low pressure recoup air from the low pressure recoup air piping to the gas turbine enclosure; and a controller operatively coupled to the first valve and the second valve to control the flow of the low pressure recoup air from the low pressure recoup air piping to the gas turbine combustion exhaust and/or the gas turbine enclosure, wherein the controller includes control logic configured to control the flow of the low pressure recoup air as a function of an ambient temperature measurement obtained about the air intake system, an air intake system temperature measurement obtained within the air intake system, and a predetermined temperature requirement having an ambient temperature constraint and an air intake system temperature differential constraint, wherein the control logic is configured to control the flow of the low pressure recoup air from the low pressure recoup air piping to the gas turbine combustion exhaust and/or the gas turbine enclosure based on values of the ambient temperature measurement and the air intake system temperature measurement in relation to satisfying the ambient temperature constraint and the combustion air intake system temperature differential constraint. a gas turbine enclosure; a gas turbine engine disposed in the gas turbine enclosure; an air intake system operatively coupled to the gas turbine enclosure to direct air to the gas turbine engine, wherein the air intake system includes an air filter house to filter the air directed to the gas turbine engine; a gas turbine combustion exhaust operatively coupled to the gas turbine engine to output an exhaust flow generated from the gas turbine engine outside of the gas turbine enclosure; low pressure recoup air piping operatively coupled to the gas turbine engine, the gas turbine enclosure and the gas turbine combustion exhaust to provide low pressure recoup air vented from the gas turbine engine to the gas turbine combustion exhaust and/or the gas turbine enclosure; a first valve operatively coupled to the low pressure recoup air piping to control a flow of the low pressure recoup air to the gas turbine combustion exhaust; a second valve operatively coupled to the low pressure recoup air piping for diverting the low pressure recoup air from the low pressure recoup air piping to the gas turbine enclosure; and a controller operatively coupled to the first valve and the second valve to control the flow of the low pressure recoup air from the low pressure recoup air piping to the gas turbine combustion exhaust and/or the gas turbine enclosure, wherein the controller includes control logic configured to control the flow of the low pressure recoup air as a function of an ambient temperature measurement obtained about the air intake system, an air intake system temperature measurement obtained within the air intake system, and a predetermined temperature requirement having an ambient temperature constraint and an air intake system temperature differential constraint, wherein the control logic is configured to control the flow of the low pressure recoup air from the low pressure recoup air piping to the gas turbine combustion exhaust and/or the gas turbine enclosure based on values of the ambient temperature measurement and the air intake system temperature measurement in relation to satisfying the ambient temperature constraint and the combustion air intake system temperature differential constraint.