The paper presents the results of determining the temperature of gas turbine plant shell. The total heat transfer from the engine is calculated. The thermal protection scheme by blowing air through the porous screen is proposed to reduce the temperature of the gas turbine plant shell as well as to reduce the total heat transfer from the engine to the surrounding compartment space.
Study of Heat Transfer from the Shell of Gas Turbine Plant and Methods of Its Thermal Protection
Russ. Aeronaut.
Russian Aeronautics ; 62 , 3 ; 463-468
2019-07-01
6 pages
Article (Journal)
Electronic Resource
English
Study of Heat Transfer from the Shell of Gas Turbine Plant and Methods of Its Thermal Protection
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