Optimization of the working process parameters of a turbofan engine of high-altitude unmanned aerial vehicle

Abstract

The article describes the methodical approach to optimize the technical appearance of a turbofan engine of a power plant of high-altitude unmanned aerial vehicle (UAV). Presented the description of the authors' mathematical model of the power plant with a turbofan engines and the results of its testing. Also presented the results of parametric and optimization studies to assess the effect of the working process parameters and the engine control programs on its thrust-economic characteristics.