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- W269593003 abstract "Report presenting an experimental investigation in the altitude test chamber on an axial-flow turbojet engine at transonic flight conditions to determine the magnitude of thrust augmentation and to ascertain the operational characteristics of a combined augmentation system. Results regarding the augmented engine performance, influence of coolant on afterburner combustion, performance losses, and operational problems are provided." @default.
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- W269593003 date "1953-02-12" @default.
- W269593003 modified "2023-09-24" @default.
- W269593003 title "Turbojet-engine thrust augmentation at altitude by combined ammonia injection into the compressor inlet and afterburning" @default.
- W269593003 hasPublicationYear "1953" @default.
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