General statement of the problem of the gas-turbine-driven compressor plant enclosure heat state and appropriate mathematical model are developed. Numerical simulation results showed that enclosure envelopes temperatures numerical evaluations are highly sensitive to the engine case outer surface temperatures and solid surfaces emissivities.
Keywords: gas-turbine, sound and heat proofing, ventilation, cooling, flow, heat and mass transfer, Reynolds averaged Navier-Stokes equations, radiation transfer equation, finite volume method, discrete ordinate method, temperature fields.