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Does anyone have any details about the engines proposed for the Boeing transonic airliner studies? I would assume that that a low bypass ratio (<2-3:1) type would have been used?Indeed, isn't a conventional high bypass ratio (4-6:1) turbofan incompatible with transonic performance?
Does anyone have any details about the engines proposed for the Boeing transonic airliner studies?
I would assume that that a low bypass ratio (<2-3:1) type would have been used?
Indeed, isn't a conventional high bypass ratio (4-6:1) turbofan incompatible with transonic performance?
