.... It is targeted use is propulsion systems optimization and design such as Turboshaft or turbofan by preparing the necessary engine functions. A number of input parameters and objective functions can be modified accordingly. The particle optimization method was introduced by Eberhart and Kennedy (1995...

...Mojtaba Tahani; Mehran Masdari; Ali Bargestan Purpose The overall performance of an aerial vehicle strongly depends on the specifics of the propulsion system and its position relative to the other components. The purpose of paper is this factor can be characterized by changing several contributing...

... and combustion characteristics. Combustion Aviation alternative fuel Compression ignition engine Propulsion system Unmanned aerial vehicle An unmanned aerial vehicle (UAV) has become one of the most active and important development directions in the field of aviation. The research on UAVs has...

... (AF) such as liquid methane and propane – butane mixture (propane – butane). This paper also assessed the efficiency of mid-flight propulsion system (PS) based on HGTE for advanced short – medium hall aircrafts (SMHA) of 2025 (with level of parameters corresponding to technologies of 2025-2030 time...