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- W4308659665 abstract "In this paper the using possibility of the scheme of an ejector turbojet engine with an afterburner (ETJEA) was carried out. The effectiveness of using of an ejector nozzle during a takeoff aircraft mode is determined. Experimental research of ETJEA were carried out on a unit with obtaining of engine thrust." @default.
- W4308659665 created "2022-11-13" @default.
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- W4308659665 date "2022-09-21" @default.
- W4308659665 modified "2023-09-27" @default.
- W4308659665 title "Research of Thrust Increase on the Ejector Turbojet Engine with the Afterburner" @default.
- W4308659665 cites W1991772348 @default.
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- W4308659665 doi "https://doi.org/10.1109/dvm55487.2022.9930931" @default.
- W4308659665 hasPublicationYear "2022" @default.
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