Abstract
All leading aviation firms in the United States of America (USA), Europe and Russia are engaged in the development of a business supersonic passenger aircraft (SPA). The authors justified the need to create a new engine for the power plant of the supersonic passenger aircraft and determined the appearance and parameters of this engine. For the first time, a study using a modern program was carried out based on the existing scientific and technical reserve on materials and efficiency of elements for a 5th generation engine with a take-off thrust of 200 kN and a gas temperature in front of the turbine of 1800 K with an increase to 2000 K as the flight speed increases. The optimal characteristics of the pressure ratio in the axial compressor (πк*) and the bypass ratio (m0) were determined and scientifically substantiated to ensure acceptable characteristics of thrust and fuel consumption at all stages of flight.
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Acknowledgements
This work is partially supported by Gadzhiev Khochbar Rasulovich, who is the associated professor and candidate of technical sciences. The authors also gratefully acknowledge the helpful comments and suggestions of the reviewers, which have improved the presentation.
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Kaligina, P.D., Leonov, D.A., Surma, A.A. (2023). Research on the Outline and Parameters Selection of the Power Plant for a Supersonic Passenger Aircraft Designed to Carry up to 20 Passengers. In: Strelets, D.Y., Korsun, O.N. (eds) Recent Developments in High-Speed Transport. Springer Aerospace Technology. Springer, Singapore. https://doi.org/10.1007/978-981-19-9010-6_9
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DOI: https://doi.org/10.1007/978-981-19-9010-6_9
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