Problems of selecting the concept and parameters of the advanced supersonic passenger air- craft propulsion system during multidisciplinary integration of the propulsion system with the airpframe
Keywords:
propulsion system, supersonic passenger aircraf, optimization, mathematical modelAbstract
The paper describes the concept formation and selection of the parameters of the propulsion system of an advanced supersonic passenger aircraft with a take-off weight of ~ 80 tons based on a multidisciplinary approach with an assessment of the main target indicators of the aircraft. The solution of the problem was carried out using a set of mathematical models which provide the calculation of the parameters of the engine, propulsion system, aircraft, as well as the flight, take-off and landing, and acoustic characteristics. The vector of rational solutions is presented in the form of a set of Pareto optimal options, from which several of the most preferable ones are selected. doi 10.54708/19926502_2024_283105116Downloads
Published
2025-08-01
Issue
Section
******************************