Shaping the GTE concept, selection of parameters and design scheme. Determination of GTE mass. Shaping the propeller concept, selection of parameters and design scheme. Determination of propeller mass

Deliverable will identify the parameters of the main engine components, the basic geometric parameters of the air-gas duct, the engine design diagram, developed a mathematical model of the engine, the choice of control laws and determined parameters in the main design points, selected design diagram of the engine, the evaluation of its mass and overall dimensions.Deliverable will also define the parameters of the propeller; the basic geometric parameters of the propeller; the method of controlling the propeller; the design scheme of the propeller, the evaluation of its mass and overall dimensions.