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Thermodynamics and aerodynamics analysis of blading system of an aerobased gas turbine/Rosilawati Abd Rahim
A two stage gas turbine is required to be designed from a standard aero-jet engine for the generation of electricity. The gas turbine in it’s is most common form is a heat engine operating by means of a series of process consist of compression of air taking from atmosphere, increase of gas temperature by the constant pressure combustion of fuel in ...
10/28/20202/1/2002Rosilawati Abd Rahim - Author
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