APLICATION OF SIMULATION ON INITIAL STAGES OF DISPOSABLE UNMANNED AERIAL VEHICLES PROPULSION SYSTEM DEVELOPMENT
The features of various means of simulation on initial stages of designing a propulsion system for disposable unmanned aerial vehicle (UAV) are discussed. Authors conducted thermogasdynamic workflow modeling of gas turbine engine for UAV using simulation system (SIM) DVIGwp. The optimization of GTE thermodynamic cycle parameters for disposable UAV is under consideration. Structural features of gas turbine engines for disposable UAV are described. Results of gasdynamic modeling of GTE compressors for disposable UAV are presented