30th Congress of the International Council of the Aeronautical Sciences

04 - Propulsion

KEY FEATURES FORECAST OF BYPASS TURBOJET ENGINE WITH MIXING FOR PERSPECTIVE AVIATION COMPLEXES

D.A. Akhmedzyanov¹, A.E. Kishalov¹, K.V. Markina¹, V.D. Lipatov¹; ¹USATU, Russia

The review and analysis of the parameters of bypass turbojet engines with afterburners for high-maneuverable turbojet aircraft were made. The engines were simulated in the system of modeling simulation Dvigw, the missing parameters and characteristics of engines were defined. There are presented trends and laws, by which the basic parameters forecast of perspective aviation engines was executed. On the base of identified regularities are predicted values of main parameters of the engine perspective.


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